University of Alabama, Huntsville PDR

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CanSat 2016 PDR Team 3822 - Skydive 1

CanSat 2016

Preliminary Design Review (PDR)

3822

UAH Space Hardware Club

Team Skydive

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Presentation Outline

bull Systems Overview ndash Lloyd Walker

bull Sensor Subsystem Design ndash Melissa Anderson

bull Descent Control Design ndash Will Barton

bull Mechanical Subsystem Design ndash Will Barton

bull CDH Subsystem Design ndash Nate Roth

bull Electrical Power System Design ndash Jarod Matlock

bull Flight Software Design ndash Eliza Dellert

bull Ground Control System ndash Beth Dutour

bull CanSat Integration and Testing ndash Nathan Endres

bull Mission Operations and Analysis ndash Eliza Dellert

bull Requirements and Compliance ndash Lloyd Walker

bull Management - Melissa Anderson

Presenter Lloyd Walker

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Team Organization


Team Lead

Lloyd Walker

Graduate Student

Software Lead

Nate Roth

Junior

Melissa Anderson

Nathan Endres

Will Barton

Eliza Dellert

Mechanical Lead

Will Barton

Junior

Lloyd Walker

Nate Roth

Melissa Anderson

Electrical Lead

Jarod Matlock

Sophomore

Nathan Endres

Junior

Eliza Dellert

Sophomore

Beth Dutour

Junior

Lloyd Walker

Faculty Advisor

Dr Wessling

CanSat Mentor

Caitlin Marsh

Alternate Team Lead

Melissa Anderson Junior

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Acronyms

bull ADC ndash Analog to Digital Converter

bull AoA ndash Angel of Attack

bull CCG ndash CanSat Competition Guide

bull CDH ndash Command and Data Handling

bull CETR ndash CanSat Environmental Testing Requirements

bull DCS ndash Descent Control System

bull LD ndash Lift to Drag ratio

bull LED ndash Light Emitting Diode

bull Li-Ion ndash Lithium Ion

bull LSB ndash Least Significant Bit

bull MCU ndash Microcontroller unit

bull Ni-Cad ndash Nickel ndash Cadmium

bull Ni-MH ndash Nickel ndash Metal Hydride

bull PCB ndash Printed Circuit Board

bull PDR ndash Preliminary Design Review

bull PT ndash Pressure Temperature Sensor

bull RBF ndash Remove Before Flight

bull RTC ndash Real Time Clock

bull SPI ndash Serial Peripheral Interface

bull GCS ndash Ground Control Station


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Systems Overview

Lloyd Walker

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Mission Summary


bull Simulate a planetary atmospheric sampling mission

using a glider

bull Provide position velocity temperature pressure and

altitude readings

bull Descend from 400 meters in a preset circular pattern

with a diameter no larger than 1000 meters

bull Bonus Objective 1 Move Camera

ndashPrevious experience with servo

ndashSimple mechanical design

bull Personal Objectives

ndashDesign a full system from concept to delivery

ndashBuild functional pitot tube

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(If You Want) System Requirement Summary

CanSat 2016 PDR Team 3822 - Skydive 7 Presenter Lloyd Walker

Requirement Number

The CanSat (container and glider) shall deploy from the rocket payload section CCG 9

The glider must be released from the container at 400 meters +- 10 m CCG 10

The glider shall not be remotely steered or autonomously steered It must be fixed to glide in a

preset circular pattern of no greater than 1000 meter diameter No active control surfaces are allowed

CCG 11

During descent the glider shall transmit all telemetry at a 1 Hz rate CCG 22

Telemetry shall include mission time with one second or better resolution which begins when the

glider is powered on Mission time shall be maintained in the event of a processor reset during the launch and mission

CCG 23

The glider shall receive a command to capture an image of the ground and store the image on board for later retrieval

CCG 43

The glider vehicle shall incorporate a pitot tube and measure the speed independent of GPS The speed shall be compared with GPS speed

CCG 45

The glide duration shall be as close to 2 minutes as possible CCG 46

A buzzer must be included that turns on after landing to aid in location CCG 48

Glider shall be a fixed wing glider No parachutes no parasails no autogyro no propellers CCG 49

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System Level CanSat Configuration

Trade amp Selection


Delta Wing Glider Monoplane Glider

Nylon stretched fabric between two rails

bull Flat Plate wing analysis

bull Simplified construction

bull Non rigid wing

Basic Hershey bar wing

bull Simplified Aerodynamic equations

bull Cambered airfoil analysis

bull Rigid wing

Choice Monoplane Glider

-Ease of analysis and rigid wing design provide higher

likelihood of mission success

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System Concept of Operations


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(If You Want) System Concept of Operations (cont)

bull Post Launch Recovery

1 Find the landing site of the payload

bullAudible beacon and GPS will ease recovery

2 Check payload

3 Insert RBF pin to power down

4 Return to ground station

5 Remove flight data

bull Data Reduction

1 Examine plotted data to show

outliers

2 Extract outliers


-Plot with outliers

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(If You Want) Physical Layout

11

Batteries and electronics will be

housed inside the fuselage below

the wings

Tail boom will extend through the

body of the fuselage and mount to

the tail plane assembly

Wings will hinge from the top of the

fuselage to allow fitting in the canister


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12

Physical Layout (cont)


Hinged Wings

Deployed

Circuit Board

Tail Boom

Fuselage

Vertical

Stabilizer

Horizontal

Stabilizer

Launch

Configuration

Battery Pack

CanSat 2016 PDR Team 3822 - Skydive

Payload Layout Container Layout

Launch

Configuration

Post Deployment

Pitot Tube

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(If You Want) Launch Vehicle Compatibility

bull Container and science vehicle

will be loaded into the payload

section of the launch vehicle

bull Prior to launch day a fit test will

be conducted

bull Container dimensions will allow

for parachute packing and easy

deployment

bull Purchasing payload section will

provide testing opportunities to

ensure proper fitting

bull Width ndash 7 mm clearance

bull Length ndash 30 mm clearance

13 CanSat 2016 PDR Team 3822 - Skydive 13 Presenter Lloyd Walker

Container

13 13

125 mm

310 mm

118 mm

280 mm

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Sensor Subsystem Design

Melissa Anderson

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(If You Want) Sensor Subsystem Overview

15

Sensor Section Part Number Description

GPS Payload M10382

Using to track position and speed

with respect to satellites also

tracks satellite number

Pressure Payload MS5611 (2) Using two sensors for pitot tube

measurements these will give

airspeed

Temperature Payload BC2309-ND Using a thermistor for outside

temperature measurements

Camera Payload 808 16 Car Keys

Micro Camera

Using to take photo on command

received from ground station

Battery Voltage Payload Voltage Divider to

ADC in MCU

Using to track battery voltage and

ensure necessary power is

supplied

Presenter Melissa Anderson CanSat 2016 PDR Team 3822 - Skydive

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Sensor Subsystem Requirements

Presenter Melissa Anderson

Requirement Number

During descent the glider shall collect air pressure outside air temperature and battery

voltage once per second

CCG 21


The glider vehicle shall incorporate a pitot tube and measure the speed independent of

GPS The speed shall be compared with GPS speed

CCG 45

Altitude needs a one meter resolution from a non-gps sensor CCG 33

The temperature is the sensed temperature in degrees C with one degree resolution CCG 33

The pressure is the measurement of atmospheric pressure CCG 33

The GPS latitude is the latitude measured by the GPS receiver CCG 33

The GPS longitude is the longitude measured by the GPS receiver CCG 33

The GPS altitude is the altitude measured by the GPS receiver CCG 33

The GPS satellite number is the number of satellites being tracked by the GPS receiver CCG 33

The GPS speed is the speed measured by the GPS receiver CCG 33

The voltage is the voltage of the CanSat power bus CCG 33

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GPS Receiver Trade amp Selection

Choice Antenova M10382

ndash Ublox 6 chip

ndash Lowest noise figure

ndash Communication interface

options


Model Pros Cons Cost

Antenova M10478 bull Horizontal accuracy lt25 m

bull 66 channels

bull SiRFstarIV 9333 chipset

bull 2 dB noise figure

$1515

Antenova M10382 bull Ublox 6 chipset


bull Multiple host interfaces

bull 50 channels $1814

RXM GPS-RM-B bull 66 channels bull MediaTek MT3337 chipset

bull Inadequate data sheet

$1934

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Air Pressure Sensor

Trade amp Selection

Choice MS5611

ndash Absolute pressure measurement

ndash Multiple interfaces

ndash Best accuracy



MS5611 bull +- 015 kPa accuracy

bull Absolute pressure

measurement

bull SPI interface

bull 21 ms for conversion time

bull Difficult to solder

$1442

MP3V5050 bull 1 ms response time

bull Simple solder

connection

bull Differential pressure

measurement

bull +- 125 kPa accuracy

bull I2C interface

bull typical voltage was 30 V

$1062

MPL115A2 bull Absolute pressure

measurement

bull +- 1 kPa

bull I2C interface


$598

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(If You Want) Pitot Tube Trade and Selection

Choice Homemade Pitot tube using MS5611

ndashCustomization possibilities

ndashFulfills a personal goal

19

Pitot Tube

Option Pros Cons Cost

Homemade Pitot tube

using MS5611

Pressure sensors

bull Atmospheric pressure can be used to

measure altitude

bull Custom fit to our payload

bull Previous workable code

bull Challenge to build

$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set

bull Subtracts the need to calculate

airspeed from pressure

bull Uses temperature to get a more

accurate airspeed reading

bull No real datasheet

could be found

bull I2C interface

$4944

Dwyer 160-8 bull No calibration needed

bull Nearly impossible to damage

bull 8-58rsquo insertion

length

$6304

CanSat 2016 PDR Team 3822 - Skydive 19 Presenter Melissa Anderson

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Air Temperature Sensor

Trade amp Selection

Choice NTCLE100E3473JB0

‒ Experience

‒ Through hole preferred for easy soldering

‒ Best accuracy


Model Pros Cons Price

NTCLE100E3473JB0 bull Through Hole

bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy

bull R25 tolerance +-

3

$039

RD4504-328-59-D1 bull Through Hole

bull Thermistor

bull R25 tolerance +- 2

bull No detailed data

sheet

bull +- 1degC accuracy

$170

AD7314ARMZ-REEL7 bull SPI communication

bull 25 micros conversion time


bull Surface Mount

$283

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Battery Voltage Sensor

Trade amp Selection

Choice Voltage Divider to ADC on MCU

‒ Easy communication

‒ Best LSB accuracy



ADC081C027CIMKNOPBCT-ND bull 3 pin SOT3

package

bull I2C


bull 100 mA consumption

$156

MAX1118EKA+TCT-ND bull 23 micros conversion

time

bull 175 microA consumption

bull SPI

bull 8 pin SOT3

package

bull +- 1 LSB accuracy

$189

Voltage Divider to ADC

on MCU

bull Direct

communication


bull 025 micros conversion

time

~$100

-MCU

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Camera Trade amp Selection

Choice 808 16 Car Keys Micro Camera

ndash Light weight (8 grams)

ndash Has on board storage

ndash Previous experience with product



Micron MT9D111 bull Automatic image

enhancement

bull Easy access to

register for storing

bull Heavy $1500

808 16 Car Keys Micro

Camera

bull Experience

bull Light weight

bull Supports up to 32Gb

of memory through a

micro SD

bull High cost $4796

OV7670 Camera Module bull Auto de-noise feature

bull Light weight

bull I2C interface $1199

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23

Descent Control Design

Will Barton


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(If You Want) Descent Control Overview

24 Presenter Will Barton CanSat 2016 PDR Team 3822 - Skydive

Altitude Canister Payload

gt 400 m Parasheet Inside

Container

400 m Deploy Glider Separate from

Container

lt 400m Parasheet Preset Circular

pattern

gt400m

400 +-10 m

lt 400m 400-0 m

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(If You Want) Descent Control Requirements

25

Payload Descent Control Requirements Number

The glider shall be completely contained in the container No part of the glider may extend beyond the container CCG 2

The glider shall not be remotely steered or autonomously steered It must be fixed to glide in a preset circular pattern of

no greater than 1000 meter diameter No active control surfaces are allowed

CCG 11

All descent control device attachment components shall survive 30 Gs of shock CCG 12

All descent control devices shall survive 30 Gs of shock CCG 13

Container Descent Control Requirements Number

Container shall fit in a cylindrical envelope of 125 mm diameter x 310 mm length including the container passive descent

control system Tolerances are to be included to facilitate container deployment from the rocket fairing

CCG 3

The container shall use a passive descent control system It cannot free fall A parachute is allowed and highly

recommended Include a spill hole to reduce swaying

CCG 4

The container must be a florescent color orange or pink CCG 6

The rocket airframe shall not be used to restrain any deployable parts of the

CanSat

CCG 7

The rocket airframe shall not be used as part of the CanSat operations CCG 8

The CanSat must deploy from the rocketrsquos payload section CCG 9

The science vehicle must be deployed at 400 m within a tolerance of +- 10 meters CCG 10

CanSat 2016 PDR Team 3822 - Skydive 25 Presenter Will Barton

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Container Descent Control Strategy

Trade and Selection

26 CanSat 2016 PDR Team 3822 - Skydive 26 Presenter Will Barton

bull Choice Nylon Parasheet with spill hole

ndash Simple due to past experience

ndash Highly recommended in the Mission Guide

bull Fluorescent orange color for high visibility

bull Connected with Kevlar cord and swivel

bull Pull and drop tests for shock testing

Descent Control

Mechanism Pros Cons

Rigid Body Parachute with

Spill Hole

bull Simple to create

bull Meets all competition requirements

bull Heavy Compared to Nylon

bull Takes up valuable space

inside rocket payload section

Nylon Parasheet with Spill

Hole


bull Past experience with this mechanism


bull Susceptible to entanglement

bull Slightly unpredictable

Built in Airbrakes bull Could potentially take up less space

than parachute

bull Being built in descent could

be considered a free-fall

bull Heavier than Nylon Parasheet

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Payload Descent Control Strategy

Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model

No zero angle of attack lift

LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg

Higher lift induced drag

Choice Cambered airfoil bull LD optimizes wing area descent

angle and bank angle

Selected Neon Red for glider color

bull Provides high visibility

Preflight Review testability

bull Test deploy wings

bull Inspect control surface angles

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(If You Want) Container Descent Rate Estimates


bull Drag equation was used to

size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)

bull Area of a circle was used to

find parasheet radius

including a spill hole of 10

of the radius

bull 119860119901 = 0991205871199031199012

bull Solving for outer radius

yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08

119860119888 Frontal Area

of Containter 001227 1198982

120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042

119907 Velocity 1 - 20 119898119904 Assumes Weight equals Drag

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Container Descent Rate Estimates

(cont)

bull To find the best radius of parachute a range of velocities was tested

bull A plot of diameter vs velocity was constructed using the equation on the

previous slide

bull Using this graph a diameter of 30 cm was selected to provide a

deployment velocity of 13 ms


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(If You Want) Payload Descent Estimation

bull Required Vertical Speed

bull119867 = 119867119879119900119865

bull Equation for Descent Angle

bull 120579 = tanminus1120783

119914119949119914119941

bull Solve for Airspeed

bull 119881infin =119867

sin 120579

bull Solve for Wing Area

bull119878 =119882

1

2120588119867

1198621198892

1198621198973

bull Solve for Cord Length

bull119888 = 119878119887

bull Equation for Bank Angle

bullΦ = tanminus1119881infin

2

119892119877

30

Variables Name Value

H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


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(If You Want) Payload Descent Estimation (cont)


bull Vertical speed

bull 119867 = 333 119898119904 bull Descent Angle

bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594

Descent trajectory shows preset circular

pattern with max radius of 250 m

released at 400m

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Mechanical Subsystem Design

Will Barton

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(If You Want) Mechanical Subsystem Overview

bull Payload consists of deployable wings

ndash25 cm length with 30 cm wing span

ndashWings will use NACA 2410 airfoil

bullMade from ABS ribs and spar

covered in doped tissue paper

ndashEach wing will pivot on a separate

axis controlled together by a servo

ndashNo lasers

bull Container

ndash118 mm x 280 mm cylinder

ndashMiddle hinging lid

ndashPolycarbonate lid and base

ndashFiberglass sides

ndashPainted a bright fluorescent orange


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Mechanical Sub-System

Requirements

Presenter Will Barton

Payload Mechanical Subsystem Requirements Number


The glider shall not be remotely steered or autonomously steered It must be fixed to glide in a preset circular pattern of no

greater than 1000 meter diameter No active control surfaces are allowed

CCG 11



Container Mechanical Subsystem Requirements Number

Container shall fit in a cylindrical envelope of 125 mm diameter x 310 mm length including the container passive

descent control system Tolerances are to be included to facilitate container deployment from the rocket fairing

CCG 3



CCG 4

The container shall not have any sharp edges to cause it to get stuck in the rocket payload section CCG 5

The container shall be a florescent color pink or orange CCG 6

The rocket airframe shall not be used to restrain any deployable parts of the CanSat CCG 7



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Mechanical Layout of Components

Trade amp Selection

bull Shoulder wing was chosen over a low or mid wing placement This was to

increase pendulum stability

bull Wing spar and rib design was chosen due to the fact that it is lighter than a solid

wing yet almost as strong


Component Options Selected Reason

Tail boom bull Carbon Fiber

bull Fiberglass

bull Wood

bull Carbon Fiber Low torsional flexibility

Wing Spar bull Wood

bull Carbon Fiber

bull ABS

bull Wood Do not need the

strength of carbon

fiber More modular

than ABS

Fuselage bull Fiberglass

bull ABS

bull Fiberglass Less bulky to provide

more interior room

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Camera Pointing Mechanism

Trade amp Selection


System Pros Cons

Direct Drive pivot bull Simple Design

bull Full Desired Range

bull Completely Exposed

Mechanical linkage bull Camera only exposed

bull More secured mounting

bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot

Choice Direct Drive pivot

- Provides full range of desired motion

- 3-D printed from ABS

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(If You Want) Material Selections


Payload Materials

bull Fuselage will be made out of fiberglass

ndashLighter than ABS

ndashUnlike carbon fiber it allows RF signal to pass through

bull Rudder and tail fin assembly will be ABS plastic

ndashDiffering fill percentages make it easy to weight properly

ndashSimple to manufacture

bull Tail boom will be made out of carbon fiber

ndashStronger than fiberglass


bull Wings will be a paper wrapped ABS ribs with wooden spar

ndashMuch lighter than full ABS wing

ndashStrong enough for our purposes

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(If You Want) Material Selections (cont)

Container Materials

bull Side wall will be made of Fiberglass

ndashCan be made thin and strong

ndashRF transparent

ndashCylinders are easy to manufacture

bull Lid and bottom will be made of polycarbonate

ndashStronger than 3-D printed ABS

ndashEasily machined with a CNC machine

bull Hinge pin will be made of brass

ndashLess susceptible to bending than aluminum

ndashLighter than stainless steel


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(If You Want) Container - Payload Interface


bull Payload will cut a monofilament from inside the container

which will open the container and deploy the payload

bull Container will open by a spring

attached above the lidrsquos hinge

bull Payload has 18 mm width and

25 mm length clearance

bull Hinged wings will then open with

use of a servo

bull Apparatus can be implemented to

prevent jostling

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(If You Want) Structure Survivability Trades

bull Electronics mounting

ndashPCBs will be secured with circuit board

standoffs and bolts

ndashThis was chosen to satisfy ndash CCG 17

bull Electronics Enclosure

ndashThe electronics will be housed within the

fiberglass fuselage of payload

ndashEpoxy potting will used to ensure extra

security and electrical insulation

bull Electronic Connections

ndashElectronic connectors will be secured

using hot glue

bull Requirements

ndashAll structures must survive 30 Gs of

shock ndash CCG 16

ndashAll structures must be built to survive 15

Gs of acceleration ndash CCG 15

bull DCS

ndashThe payload will use metal hinge

pins

ndashThe container will use knotted

Kevlar cord

ndashNo Pyrotechnics


DCS

Attachment Pros Cons

Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)

bull Cheap bull Hard to work

with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)

bull Lighter bull Harder to

manufacture

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Mass Budget


Container

Part Mass Method

Sides 93 g Modeled

TopBottom 46 g Modeled

Descent control 14 g Estimated

Margin (10) 15 g

Total 168 g

Payload

Part Mass Method

Fuselage 85 g Estimated

Wings 35 g Estimated

Boom 16 g Estimated

Tail 20 g Estimated

Electronics 116 g Estimated

Margin (20) 54g

Total 326g Total Allocated Mass = 500 +-10 g

Total Mass = 494g

Methods for correcting mass

- If mass lt 490g ballast will be added to container

- If mass gt 510g mass will be removed from container sides

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Communication and Data Handling

(CDH) Subsystem Design

Nate Roth

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CDH Overview

Presenter Nate Roth

Part Type Part Number Function

Antenna FXP290070100A Enhance radio capabilities

Radio XBP9B-DMST-002 Transmit and receive

commands

MCU ATXMEGA128A4U

Processes all flight software

commands and prepares data

for radio transmission

Memory M25PE80-VMN6TP Stores data for post

processing

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CDH Requirements

Presenter Nate Roth

Telemetry Requirements Number



CCRG 21

During descent the glider shall transmit all telemetry at a 1 Hz rate CCRG 22

Telemetry shall include mission time with one second or better resolution which begins when

the glider is powered on and maintained in the event of a processor reset during the mission

CCRG 23

All telemetry shall be displayed in real time during descent CCRG 31

All telemetry shall be displayed in engineering units (meters meterssec Celsius etc) CCRG 32

Teams shall plot data in real time during flight CCRG 33

The telemetry shall indicate the time the last imaging command was received and the number

of commands received

CCRG 44

XBEE Requirements Number

XBEE radios shall be used for telemetry 24 GHz Series 1 and 2 radios are allowed 900

MHz XBEE Pro radios are also allowed

CCRG 24

XBEE radios shall have their NETIDPANID set to their team number CCRG 25

XBEE radios shall not use broadcast mode CCRG 26

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Processor amp Memory

Trade amp Selection

Manufacturer Model Flash

(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144

Atmel ATXMEGA128A4U 128 34 8

USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48

Choice ATXMEGA128A4U

‒ Less pins to solder

‒ Experience with chipset

‒ Internal RTC

CanSat 2016 PDR Team 3822 - Skydive 45 Presenter Nate Roth

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Trade amp Selection (cont)

Manufacturer Model Storage

Size Interface Size (mm2) Type Max Frequency (MHz)

Adesto AT25SF041-

SSHD-T 4MB SPI 30 Flash 104

Micron M25PE80-

VMN6TP 8MB SPI 30 Flash 75

Panasonic RP-

SMLF08DA1 8GB SPI 165 Flash 25

Choice M25PE80-VMN6TP

‒ Larger storage for high resolution data

‒ Small size


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(If You Want) Real-Time Clock


Type Manufacturer Operating

Frequency (Hz) Interface Features

External NXP 32 I2C

Variable frequency

setting

Built In Atmel 32 SPI Immediate integration

Choice Built In

ndash Immediate integration

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Antenna Trade amp Selection

Choice 900MHz Duck Antenna

ndash Easy to connect

ndash Same connector as the radio

Presenter Nate Roth

Model Range Polarization Gain Length Price

FXP290 902MHz ndash 928MHz Linear 15 dBi 75 cm $1631

900 MHz Mad

Mushroom

Wide range Circular 15 dBi 5 cm $4499

APAMS - 104 890MHz ndash 960MHz Linear 25 dBi 1095 cm $908

900MHz Duck

Antenna

900 MHz Linear 2 dBi 105 cm $795

900MHz Duck

Antenna

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(If You Want)


Radio Configuration

Presenter Nate Roth

bull Radio Requirements

ndashMust be a XBEE radio that is either 24Ghz (Series 1 and 2) or 900MHz Pro

ndashNETIDPANID must be set to the team number

ndashCannot be used in broadcast mode

bull Protocol and Configuration

ndashXBEE Pro 900MHz will be used

bull NETID will be set to 3822

bull Unicast mode will be used for data transmission

bull The MCU will handle the transmission rate of 1 HZ through all mission

phases

bull Testing of the radio configuration and transmission will reveal any errors

Team Logo

Here

(If You Want) Telemetry Format

bull Telemetry includes

ndash ltTEAM IDgt is the identification assigned to our team

ndash ltMISSION TIMEgt is the time since power up in seconds

ndash PACKET COUNTgt is the number of packets that have been transmitted

ndash ltALT SENSORgt is the altitude measured by a non-gps sensor with one a meter resolution

ndash ltPRESSUREgt is the measurement of atmospheric pressure

ndash ltSPEEDgt is the speed in meterssec and is derived from the pitot tube

ndash ltTEMPgt is the temperature in Celsius with a one degree resolution

ndash ltVOLTAGEgt is the voltage measured from the CanSatrsquos power bus

ndash ltGPS LATITUDEgt is the GPS receiver measured latitude

ndash ltGPS LONGITUDEgtis the GPS receiver measured longitude

ndash ltGPS ALTITUDEgt is the GPS receiver measured altitude

ndash ltGPS SAT NUMgt is the number of satellites being tracked by the GPS receiver

ndash ltGPS SPEEDgt is the GPS receiver measured speed

ndash ltCOMMAND TIMEgt is the time the most recent imaging command was received by the glider

ndash ltCOMMAND COUNTgt is the number of imaging commands the glider has received

ndash ltBONUS CAMERA FACINGgt is current angle the camera is facing

50 Presenter Nate Roth CanSat 2016 PDR Team 3822 - Skydive

Team Logo

Here

(If You Want)


Telemetry Format (cont)

bull Telemetry sent should be sent with ASCII in the below

format

ltTEAM IDgtltMISSION TIMEgtltPACKET COUNTgtltALT

SENSORgtltPRESSUREgt ltSPEEDgtltTEMPgtltVOLTAGEgtltGPS

LATITUDEgtltGPS LONGITUDEgtltGPS ALTITUDEgtltGPS SAT

NUMgt ltGPS SPEEDgtltCOMMAND TIMEgtltCOMMAND

COUNTgtltBONUS CAMERA FACINGgt

bull The transmission shall be sent at a rate of 1Hz continuously once the

CanSat is powered up

bull The payload telemetry will be saved as a comma separated file (csv)

for viewing in Excel by the judges

Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here


Electrical Power Subsystem (EPS)

Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview

Presenter Jarod Matlock

bull Battery (3V Surefire)

ndashPower source

bull Xbee Pro 900

ndashTransmit telemetry data

bull MS5611 Sensor

ndash Measure both pressure and

temperature

bull Voltage Regulator

ndashRegulate voltage from power

source to system

bull Thermistor

ndashRecord outside air temperature

Payload EPS Descriptions

bull Camera

ndashTake pictures of flight

bull GPS

ndashTransmits telemetry data

bull Switch

ndashRemove before flight accessible

through hole

Team Logo

Here

(If You Want)

CanSat 2016 PDR Team 3822 - Skydive 54 Presenter Jarod Matlock

Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here

(If You Want) EPS Overview (cont)

55

No Electrical System for Container

Team Logo

Here

(If You Want)


EPS Requirements


EPS Requirements Number

All electronic components shall be enclosed and shielded from the environment with the exception of sensors CCG 14

All electronics shall be hard mounted using proper mounts such as standoffs screws or high performance

adhesives

CCG 17

During descent the glider shall collect air pressure outside air temperature and battery voltage once per

second

CCG 21

The glider shall have an imaging camera installed and pointing toward the ground CCG 27

No lasers allowed CCG 38

The glider must include an easily accessible power switch which does not require removal from the container

for access Access hole or panel in the container is allowed

CCG 39

The glider must include a battery that is well secured to power the glider CCG 40

Lithium polymer cells are not allowed due to being a fire hazard CCG 41

Alkaline Ni-MH lithium ion built with a metal case and Ni-Cad cells are allowed Other types must be

approved before use

CCG 42

The glider vehicle shall incorporate a pitot tube and measure the speed independent of GPS The speed shall

be compared with GPS speed

CCG 45


Team Logo

Here

(If You Want)


Electrical Block Diagram


Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here

(If You Want) Payload Battery Trade amp Selection


Model Pros Cons

Surefire (Lithium Ion

Battery)

bull 3 nominal volts per cell

bull High amperage

bull Can become very hot and suffer

thermal runaway and even eruption if

mishandled

Nickel Metal Hydroxide

(Ni-MH)

bull Rechargeable making them

better equipped for high drain

components (ie cameras)


bull Short life span

Nickel Cadmium (Ni-Cd) bull Performs better at lower

temperatures




bull Cadmium based (HealthEnvironmental

Concerns)


Choice Surefire 123A

ndash3 nominal volts per cell

ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget


Component Duty Cycle Voltage Current Power Uncertainty

MS5611 PT

Sensor 100 36 V 14 mA 504 mW Datasheet

808 16 Mobius

Camera 1 5 V 300 mA 1500 mW Datasheet

XBEE Radio

(transmit) 10 34 V 215 mA 731 mW Datasheet

XBEE Radio

(receive) 90 34 V 55 mA 187 mW Datasheet

Atmel

AT32UC3A0128-

ALUR

100 36 V 125 mA 45 mW Datasheet

M10382-A1 GPS 100 36 V 10 mA 36 mW Datasheet

Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904

Using 2 Surfire 123A

Team Logo

Here

(If You Want)


Power Bus Voltage Measurement

Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here


Flight Software (FSW) Design

Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview

bull Basic FSW Architecture

ndash The flight software for this CanSat contains one main file with several

driver files

bull Programming Languages

ndash The C programming language was used to write the software for this

CanSat

bull Development Environments

ndash Atmel Studio will be used to develop the software for this CanSat

bull Software Task Summary

ndash Measure air pressure air temperature altitude velocity GPS data

and voltage

ndash Drive nichrome wire for releases

ndash Transmit flight telemetry at a rate of 1 Hz

ndash Change flight states

ndash Packet count and mission time

Presenter Eliza Dellert

Team Logo

Here

(If You Want)


FSW Requirements


FSW Requirements Number



CCG 21

Telemetry shall be transmitted at a 1 Hz rate CCG 22

Telemetry shall include mission time which is maintained in the event of a processor reset

and begins when the glider is powered on

CCG 23

Telemetry shall be displayed in real time during descent CCG 31

Telemetry will be displayed in engineering units CCG 32

Telemetry shall include an incrementing packet count which shall be maintained through

processor resets

CCG 37

Glider shall receive a command to capture an image and store the image on board CCG 43

Telemetry shall indicate the time the imaging command was received and the number of

commands received

CCG 44

Team Logo

Here

(If You Want)


CanSat FSW State Diagram


POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to

receiverdquo message

PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data

Continue real time plotting

Altitude is

400 meters

or less

GLIDER DESCENT

Turn on and off glider hot wire

from sensor or command

Send data at 1 Hz

Collect data


Execute camera commands

Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here

(If You Want) CanSat FSW State Diagram (cont)

FSW recovery

ndashWe will use on board storage to switch to the correct

flight state in case of a processor reset

ndashOn board storage will be the Micron flash memory

ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity

bullMission start time

65 CanSat 2016 PDR Team 3822 - Skydive 65 Presenter Eliza Dellert

Team Logo

Here

(If You Want)

CanSat 2016 PDR Team 3822 - Skydive 66 Presenter Eliza Dellert

Determining Altitude

calculateAltitude(pressure temperature)

determine the pressure ratio and take the logarithm of it

if the pressure ratio is negative multiply it by -1

multiply the pressure ratio by the temperature and the gas constant

divide it by the gravity and thatrsquos the final altitude

Determining Velocity

calculateVelocity(staticPres stagPres)

assume air density is constant 1225 kgm^3

vel = sqrt(2density(stagPres-staticPres)

Driving Hotwire at Glider Deploy

once the altitude is no longer greater than 400 meters drive the hotwire high

wait 5 seconds

drive the hotwire low

Glider FSW Plan

Team Logo

Here

(If You Want)


Software Development Plan


Collect functional code

used in previous projects

Assemble electrical

prototype and then start

testing and debugging

code

GPS and data storage

will be implemented first

to allow full telemetry

testing on rocket

launches

Set synchronous

milestones with electrical

team With these methods in

mind we should have a

functional flight

software by the time

the first physical

prototype is complete

and ready for testing

This allows immediate support

for the thermistor MS5611

and radio

During this stage team

members will be assigned to

research and improve upon a

component to insure efficiency

Once new electrical builds are

completed we will test code for

the added components

Team Logo

Here

(If You Want)

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Here


Ground Control System (GCS) Design

Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview

Presenter Beth Dutour

Payload

XBEE Pro on

payload

Payload

antenna

GCS antenna GCS XBEE Pro

GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here

(If You Want) GCS Requirements

70

GCS Requirements Numbers

Each team must construct their own ground station CCG 30

All telemetry shall be displayed in real time during descent CCG 31

All telemetry shall be displayed in SI engineering units CCG 32

Teams shall plot data in real time during flight CCG 33

The ground station must be comprised of a laptop with at least 2 hours of battery life an XBEE

radio and a hand held antenna

CCG 34

The ground station must be portable so that it can be moved to the ground station operation

center which is along the flight line AC power will not be available at this position

CCG 35

CanSat 2016 PDR Team 3822 - Skydive 70 Presenter Beth Dutour

Team Logo

Here

(If You Want) GCS Antenna Trade amp Selection

71 CanSat 2016 PDR Team 3822 - Skydive 71 Presenter Beth Dutour

Antenna Pros Cons

Laird Technologies PC906N Yagi

Antenna

bull Receiver gain +11 dBi

bull Experience with Yagi

antennas

bull 629 cm long

bull Will need to point in direction

of the payload

Video Aerial Systems

Mad Mushroom (MM-900)

bull Large radiation pattern bull Right hand circular

polarization

bull Choice Laird Technologies PC906N Yagi Antenna

Laird PC906N Yagi

‒ Linear polarization to better match payloadrsquos

antenna

‒ Member of the GS team will point hold the

antenna in the direction of the science vehicle

and adjust as necessary

‒ Experience

Team Logo

Here

(If You Want)

GCS Antenna Trade amp Selection

(cont)


bull Equation used for gain calculations below all values in dB

Received Power = Transmitter Output + Transmitter antenna gain + Receiver

Antenna Gain ndash Free Space Loss ndash Miscellaneous Loss

bull Received Power Xbee radio has sensitivity of -101 dBm to get a stable

connection a margin of 20 dBm was used

bull Transmitter Output Xbee Pro sb3 transmission power output is 24 dBm

bull Transmitter Antenna Gain Using a Mad Mushroom gain was 2 dBm

bull Free Space Loss Loss = 20log(frequency in MHz) + 20log(distance in km)

+3245 dB using a max distance of 3 km a value of 10108 dB is found

bull Miscellaneous Losses Loses due to wiring etc A value of 10 dB was used

bull Receiver Gain 159 dB

Team Logo

Here

(If You Want) GCS Software


bull RealTerm terminal will be used to display all telemetry data

bull Telemetry data will be stored on the ground station computer in a csv

file

bull The data will be plotted in real time using Microsoft Excelrsquos built in real

time data collection and manipulation tool

bull Graph plots will be marked with a legend and color coordinated to

improve readability

bull RealTerm will save data in a csv on the ground station laptop which will

then be accessed by Excel

Team Logo

Here

(If You Want) GCS Software (cont)


Team Logo

Here

(If You Want)

Team Logo

Here


CanSat Integration and Testing

Nathan Endres

Team Logo

Here

(If You Want)


CanSat Integration and Test

Overview

Subsystem Testing

Mechanical Testing

bull Drop tests will be used to verify descent rates structure stability

and proper circulation pattern

ndash Lower altitude tests (10-30 m) bull Dropped from a quad copter or multistory building

bull Record these drops to analyze them at a later date

bull Use a timer to estimate velocities

bull Tests durability of mechanics

ndash Higher altitude tests (500-700 m) bull Deployed from rocket

bull Tests electronics and their durability

bull Tests durability of the glider

bull Tests glider release

bull Pitot tube tests

ndash Road velocity tests bull Tests pitot tube accuracy

bull Drive with windows down and place the pitot tube in the wind stream

bull Can compare to car

Presenter Nathan Endres

2015 CanSat team GroundPounder

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing

bull Altitude calculations

ndash Walk up and down stairs

ndash Check to see if altitude changed

ndash Other ways vacuum chambers rocket launches quad copter tests

bull Verify circuitry

ndash Breadboard

ndash Design spark for PCB spacing design

bull XBEE tests

ndash Send telemetry during rocket launches

ndash Verify communication at ground station

FSW tests

bull Real time plotting

ndash Rocket launch data


Team Logo

Here

(If You Want)



Overview

Environmental Testing Drop Test Procedure (CETR 22)

1 Secure the cord to the ceiling or structure eye-bolt

2 Secure the other end of the cord to the parachute attachment point of the

container

3 Raise the CanSat up 80 cm in line with the cord

4 Release the CanSat and let it drop

5 Observe the results of the drop test Did the parachute attachment point

fail Did the science vehicle release from the container

6 Remove the science vehicle from the container and inspect for any

damage

7 If there was no damage turn on the science vehicle and perform a

functional test


Team Logo

Here

(If You Want)



Overview

Environmental Testing Vibration Test Procedure (CETR 32) 1 Perform a functional test of the CanSat

2 Mount the science vehicle on the vibration fixture and secure it in place

3 If included start the accelerometer data collection

4 Over a 1 minute period turn the sander on Let it power up to full speed

wait 2 seconds and turn off As soon as the sander stops moving repeat

until one minute is complete

5 Remove CanSat from test fixture and inspect it for any damage

6 Perform a functional test

7 Review accelerometer data to determine the intensity of the vibrations


Team Logo

Here

(If You Want)



Overview

Environmental Testing Thermal Test Procedure (CETR 42) 1 Place CanSat into the thermal chamber

2 Turn on the CanSat

3 Close and seal the thermal chamber

4 Turn on the heat source

5 Monitor the temperature and turn off the heat source when the internal

temperature reaches 60C and turn on heat source when the temperature

drops to 55C

6 Maintain the temperature for two hours

7 Turn off heat source and perform visual inspection and any functional

tests to verify the CanSat survived the thermal exposure and can operate

as expected

8 With the CanSat still hot test any mechanisms and structures to make

sure the integrity has not been compromised

9 Verify epoxy joints and composite materials still maintain their strengths


Team Logo

Here

(If You Want)



Overview


Integration

Design and Construct CanSat

bull Design container to fit constraints of the rocket

bull Design payload to fit inside of container and house all components in their necessary location

Design PCB

bull Fit PCB sensors and all other components into payload

Develop FSW

bull FSW will determine flight states and command electronics from sensor readings

bull Data will be programmed to broadcast via radio to the ground station

bull Determine the level of accuracy and optimize efficiency of data

Build Ground Station

bull Will receive FSW data via radio

bull Ground Station will coordinate display and record data

Team Logo

Here

(If You Want)

Team Logo

Here


Mission Operations amp Analysis

Eliza Dellert

Team Logo

Here

(If You Want)


Overview of Mission Sequence of

Events


Arrive at launch site

Prepare CanSat for turn in

CanSat crew

Set up ground station

GS team

Fit check

CanSat crew

Weight check

CanSat crew

Perform antenna check

GS team

Verify ground station

communication

GS team

Assemble CanSat

CanSat crew

Load CanSat into rocket

CanSat crew

Install rocket onto launch

pad

CanSat crew

Execute launch procedures

Mission Control Officer

Perform all required flight

operations

Ground station clear out

GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres

ndash Melissa Anderson

bull Mission Control Officer Lloyd Walker

bull Recovery Officer Melissa Anderson

Team Logo

Here

(If You Want)



Events (cont)


Antenna and Ground System Set-Up

bull Turn on laptop and launch RealTerm

and Excel

bull Check if receiving any data

bull Send test command to check

transmission

bull Receive test command to test receiver

bull Begin data receiving

CanSat Assembly and Test

bull Fit check

bull Place Glider into container

bull Take out RBF pin

bull Check if LEDs are flashing

bull Check if transmitting data (coordinate

with GS)

Team Logo

Here

(If You Want)


bull 2 copies of procedures are needed (CCG 64)

ndash Pages should be numbered

ndash Three ring binder

ndash Content

bull Table of Contents

bull Checklists

ndashConfiguring the ground station

ndashPreparing the CanSat

ndashAntenna setup

ndashCanSat assembly test

ndashIntegrating the CanSat into the rocket bull Procedures

ndashLaunch preparation

ndashLaunch

ndashRemoval ndash Purpose

bull Increase safety

bull Inform officials of procedures

bull Optimize team performance


Mission Operations Manual

Development Plan

86

Team Logo

Here

(If You Want)


CanSat Location and Recovery

bull CanSat will be visually tracked to the best of our ability

ndash Final position known with GPS

bull Recovery crew will split in two

ndash One group searches for the container

ndash One group searches for the payload

bull Payload signals audible beacon upon landing

bull Container will be fluorescent orange (CCG 6)

bull All CanSat components will be labeled as follows (CCG 36)

CanSat 2016 SkyDive


Contact spaceuahedu

301 Sparkman Drive Northwest Huntsville AL 35899


Team Logo

Here

(If You Want)

Team Logo

Here

CanSat 2016 CDR Team 3822 - Skydive 88

Requirements Compliance

Lloyd Walker

Team Logo

Here

(If You Want) Requirements Compliance Overview

bull Currently our design complies to each requirement

bull Some revisions may need to be made to wing

deployment

bull We will be closely tracking the mass of the CanSat

CanSat 2016 CDR Team 3822 - Skydive 89 Presenter Lloyd Walker

Team Logo

Here

(If You Want) Requirements Compliance

90 Presenter Lloyd Walker

Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes

1 Total mass of the CanSat (container and payload) shall be 500

grams +- 10 grams Comply 41 Carefully tracked

2 The glider shall be completely contained in the container No part of

the glider may extend beyond the container

Comply

13

3

Container shall fit in a cylindrical envelope of 125 mm diameter x

310 mm length including the container passive descent control

system Tolerances are to be included to facilitate container

deployment from the rocket fairing

Comply

13

Is that outer diameter or container The

payload bay fits a larger container

4

The container shall use a passive descent control system It cannot

free fall A parachute is allowed and highly recommended Include

a spill hole to reduce swaying

Comply

26

5 The container shall not have any sharp edges to cause it to get

stuck in the rocket payload section

Comply

13

6 The container must be a florescent color pink or orange Comply 26

7 The rocket airframe shall not be used to restrain any deployable

parts of the CanSat

Comply

13

8 The rocket airframe shall not be used as part of the CanSat

operations

Comply

13

9 The CanSat (container and glider) shall deploy from the rocket

payload section

Comply

13

10 The glider must be released from the container at 400 meters +-

10 m

Comply

9

11

The glider shall not be remotely steered or autonomously steered

It must be fixed to glide in a preset circular pattern of no greater

than 1000 meter diameter No active control surfaces are allowed

Comply

3031 What dictates the

diameter of the pattern (Tangent to deploy)


Team Logo

Here

(If You Want) Requirements Compliance (Cont)


Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes

12 All descent control device attachment components shall survive 30

Gs of shock Comply 40

13 All descent control devices shall survive 30 Gs of shock Comply 40

14 All electronic components shall be enclosed and shielded from the

environment with the exception of sensors

Comply

40

15 All structures shall be built to survive 15 Gs acceleration Comply 40

16 All structures shall be built to survive 30 Gs of shock Comply 40

17 All electronics shall be hard mounted using proper mounts such as

standoffs screws or high performance adhesives Comply 40

18 All mechanisms shall be capable of maintaining their configuration

or states under all forces Comply 40

19 Mechanisms shall not use pyrotechnics or chemicals Comply 40

20

Mechanisms that use heat (eg nichrome wire) shall not be

exposed to the outside environment to reduce potential risk of

setting vegetation on fire

Comply 40

21 During descent the glider shall collect air pressure outside air

temperature and battery voltage once per second Comply 15

22 During descent the glider shall transmit all telemetry at a 1 Hz rate Comply 51

23

Telemetry shall include mission time with one second or better

resolution which begins when the glider is powered on Mission

time shall be maintained in the event of a processor reset during

the launch and mission

Comply 51

24 XBEE radios shall be used for telemetry 24 GHz Series 1 and 2

radios are allowed 900 MHz XBEE Pro radios are also allowed Comply 49


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes

25 XBEE radios shall have their NETIDPANID set to their team

number Comply 49

26 XBEE radios shall not use broadcast mode Comply 49

27 The glider shall have an imaging camera installed and pointing

toward the ground

Comply

36

28 The resolution of the camera shall be a minimum of 640x480 pixels

in color Comply 22

29 Cost of the CanSat shall be under $1000 Ground support and

analysis tools are not included in the cost Comply 9596

30 Each team shall develop their own ground station Comply 69

31 All telemetry shall be displayed in real time during descent Comply 73

32 All telemetry shall be displayed in engineering units (meters

meterssec Celsius etc) Comply 74

33 Teams shall plot data in real time during flight Comply 73

34

The ground station shall include one laptop computer with a

minimum of two hours of battery operation xbee radio and a hand

held antenna

Comply 69

35

The ground station must be portable so the team can be positioned

at the ground station operation site along the flight line AC power

will not be available at the ground station operation site

Comply 69

36 Both the container and glider shall be labeled with team contact

information including email address Comply 87

37

The flight software shall maintain a count of packets transmitted

which shall increment with each packet transmission throughout the

mission The value shall be maintained through processor resets

Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes

38 No lasers allowed Comply 33

39

The glider must include an easily accessible power switch which

does not require removal from the container for access Access

hole or panel in the container is allowed

Comply 55

40 The glider must include a battery that is well secured to power the

glider

Comply

4055

41 Lithium polymer cells are not allowed due to being a fire hazard Comply 58

42 Alkaline Ni-MH lithium ion built with a metal case and Ni-Cad cells

are allowed Other types must be approved before use Comply 58

43 The glider shall receive a command to capture an image of the

ground and store the image on board for later retrieval Comply 64

44 The telemetry shall indicate the time the last imaging command

was received and the number of commands received Comply 50

45

The glider vehicle shall incorporate a pitot tube and measure the

speed independent of GPS The speed shall be compared with

GPS speed

Comply 19

46 The glide duration shall be as close to 2 minutes as possible Comply 3031

47

The CanSat shall have a payload release override command to

force the release of the payload in case the autonomous release

fails

Comply 64

48 A buzzer must be included that turns on after landing to aid in

location Comply 55

49 Glider shall be a fixed wing glider No parachutes no parasails no

auto-gyro no propellers Comply 8


Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)


CanSat Budget ndash Hardware


Subsystem Component Cost

Sensors MS5611 (2) $2882 - Actual

Sensors M10382 $1814 - Actual

Sensors 808 16V3 $4796 - Actual

CDH AT32UC3A0128-ALUR $1192 - Actual

CDH XBEE Pro $5369 - Actual

CDH 900MHz Duck Antenna $795 - Actual

Descent Control Ripstop Nylon $1598 - Actual

Descent Control Kevlar Chord $899 - Actual

Descent Control Springs $722 - Actual

Mechanical ABS $20 - Estimate

Mechanical Screws $2 - Estimate

Mechanical Polycarbonate $15 - Estimate

Team Logo

Here

(If You Want)


CanSat Budget ndash Hardware (cont)



EPS Buzzer $354 - Actual

EPS Mosfets $084 - Actual

EPS Thermistor $039 - Actual

EPS PCB $33 - Estimate

EPS Capacitors $400 - Estimate

EPS Resistors $300 - Estimate

Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)


CanSat Budget ndash Other Costs


Subsystem Component Cost-Actual

GCS Mounting Hardware $50-Estimate

GCS XBEE $3350 - Actual

GCS Laird Technologies PC906N Yagi

Antenna

$3895 - Actual

Other Rocket Launch Hardware $150-Estimate

Other Testing and Prototypes $450-Estimate

Other Rapid Prototyping ABS $125-Estimate

Other Travel $4750- Estimate

Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)


Program Schedule (cont)


Team Logo

Here

(If You Want)


Conclusions

bull Mission design has been completed

ndash Mechanical Payload and container design complete

ndash Software Pitot tube and GPS programming has begun

ndash Electric Electrical schematics and parts have been

chosen

bull Next step Implementation

ndash Mechanical Build first prototypes

ndash Software Finish and test GPS and pitot tube

ndash Electric PCB design


Team Logo

Here

(If You Want)


Presentation Outline

bull Systems Overview ndash Lloyd Walker

bull Sensor Subsystem Design ndash Melissa Anderson

bull Descent Control Design ndash Will Barton

bull Mechanical Subsystem Design ndash Will Barton

bull CDH Subsystem Design ndash Nate Roth

bull Electrical Power System Design ndash Jarod Matlock

bull Flight Software Design ndash Eliza Dellert

bull Ground Control System ndash Beth Dutour

bull CanSat Integration and Testing ndash Nathan Endres

bull Mission Operations and Analysis ndash Eliza Dellert

bull Requirements and Compliance ndash Lloyd Walker

bull Management - Melissa Anderson


Team Logo

Here

(If You Want)


Team Organization


Team Lead

Lloyd Walker

Graduate Student

Software Lead

Nate Roth

Junior

Melissa Anderson

Nathan Endres

Will Barton

Eliza Dellert

Mechanical Lead

Will Barton

Junior

Lloyd Walker

Nate Roth

Melissa Anderson

Electrical Lead

Jarod Matlock

Sophomore

Nathan Endres

Junior

Eliza Dellert

Sophomore

Beth Dutour

Junior

Lloyd Walker

Faculty Advisor

Dr Wessling

CanSat Mentor

Caitlin Marsh

Alternate Team Lead


Team Logo

Here

(If You Want)


Acronyms






















Team Logo

Here

(If You Want)

Team Logo

Here


Systems Overview

Lloyd Walker

Team Logo

Here

(If You Want)


Mission Summary



using a glider


altitude readings









Team Logo

Here



Requirement Number





CCG 11




CCG 23


CCG 43


CCG 45




Team Logo

Here

(If You Want)



Trade amp Selection






bull Non rigid wing




bull Rigid wing




Team Logo

Here

(If You Want)




Team Logo

Here





2 Check payload




bull Data Reduction


outliers

2 Extract outliers


-Plot with outliers

Team Logo

Here


11



the wings







Team Logo

Here

(If You Want)

12



Hinged Wings

Deployed

Circuit Board

Tail Boom

Fuselage

Vertical

Stabilizer

Horizontal

Stabilizer

Launch

Configuration

Battery Pack



Launch

Configuration

Post Deployment

Pitot Tube

Team Logo

Here






be conducted



deployment







Container

13 13

125 mm

310 mm

118 mm

280 mm

Team Logo

Here

(If You Want)

Team Logo

Here



Melissa Anderson

Team Logo

Here


15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


Team Organization


Team Lead

Lloyd Walker

Graduate Student

Software Lead

Nate Roth

Junior

Melissa Anderson

Nathan Endres

Will Barton

Eliza Dellert

Mechanical Lead

Will Barton

Junior

Lloyd Walker

Nate Roth

Melissa Anderson

Electrical Lead

Jarod Matlock

Sophomore

Nathan Endres

Junior

Eliza Dellert

Sophomore

Beth Dutour

Junior

Lloyd Walker

Faculty Advisor

Dr Wessling

CanSat Mentor

Caitlin Marsh

Alternate Team Lead


Team Logo

Here

(If You Want)


Acronyms






















Team Logo

Here

(If You Want)

Team Logo

Here


Systems Overview

Lloyd Walker

Team Logo

Here

(If You Want)


Mission Summary



using a glider


altitude readings









Team Logo

Here



Requirement Number





CCG 11




CCG 23


CCG 43


CCG 45




Team Logo

Here

(If You Want)



Trade amp Selection






bull Non rigid wing




bull Rigid wing




Team Logo

Here

(If You Want)




Team Logo

Here





2 Check payload




bull Data Reduction


outliers

2 Extract outliers


-Plot with outliers

Team Logo

Here


11



the wings







Team Logo

Here

(If You Want)

12



Hinged Wings

Deployed

Circuit Board

Tail Boom

Fuselage

Vertical

Stabilizer

Horizontal

Stabilizer

Launch

Configuration

Battery Pack



Launch

Configuration

Post Deployment

Pitot Tube

Team Logo

Here






be conducted



deployment







Container

13 13

125 mm

310 mm

118 mm

280 mm

Team Logo

Here

(If You Want)

Team Logo

Here



Melissa Anderson

Team Logo

Here


15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


Acronyms






















Team Logo

Here

(If You Want)

Team Logo

Here


Systems Overview

Lloyd Walker

Team Logo

Here

(If You Want)


Mission Summary



using a glider


altitude readings









Team Logo

Here



Requirement Number





CCG 11




CCG 23


CCG 43


CCG 45




Team Logo

Here

(If You Want)



Trade amp Selection






bull Non rigid wing




bull Rigid wing




Team Logo

Here

(If You Want)




Team Logo

Here





2 Check payload




bull Data Reduction


outliers

2 Extract outliers


-Plot with outliers

Team Logo

Here


11



the wings







Team Logo

Here

(If You Want)

12



Hinged Wings

Deployed

Circuit Board

Tail Boom

Fuselage

Vertical

Stabilizer

Horizontal

Stabilizer

Launch

Configuration

Battery Pack



Launch

Configuration

Post Deployment

Pitot Tube

Team Logo

Here






be conducted



deployment







Container

13 13

125 mm

310 mm

118 mm

280 mm

Team Logo

Here

(If You Want)

Team Logo

Here



Melissa Anderson

Team Logo

Here


15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

Team Logo

Here


Systems Overview

Lloyd Walker

Team Logo

Here

(If You Want)


Mission Summary



using a glider


altitude readings









Team Logo

Here



Requirement Number





CCG 11




CCG 23


CCG 43


CCG 45




Team Logo

Here

(If You Want)



Trade amp Selection






bull Non rigid wing




bull Rigid wing




Team Logo

Here

(If You Want)




Team Logo

Here





2 Check payload




bull Data Reduction


outliers

2 Extract outliers


-Plot with outliers

Team Logo

Here


11



the wings







Team Logo

Here

(If You Want)

12



Hinged Wings

Deployed

Circuit Board

Tail Boom

Fuselage

Vertical

Stabilizer

Horizontal

Stabilizer

Launch

Configuration

Battery Pack



Launch

Configuration

Post Deployment

Pitot Tube

Team Logo

Here






be conducted



deployment







Container

13 13

125 mm

310 mm

118 mm

280 mm

Team Logo

Here

(If You Want)

Team Logo

Here



Melissa Anderson

Team Logo

Here


15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


Mission Summary



using a glider


altitude readings









Team Logo

Here



Requirement Number





CCG 11




CCG 23


CCG 43


CCG 45




Team Logo

Here

(If You Want)



Trade amp Selection






bull Non rigid wing




bull Rigid wing




Team Logo

Here

(If You Want)




Team Logo

Here





2 Check payload




bull Data Reduction


outliers

2 Extract outliers


-Plot with outliers

Team Logo

Here


11



the wings







Team Logo

Here

(If You Want)

12



Hinged Wings

Deployed

Circuit Board

Tail Boom

Fuselage

Vertical

Stabilizer

Horizontal

Stabilizer

Launch

Configuration

Battery Pack



Launch

Configuration

Post Deployment

Pitot Tube

Team Logo

Here






be conducted



deployment







Container

13 13

125 mm

310 mm

118 mm

280 mm

Team Logo

Here

(If You Want)

Team Logo

Here



Melissa Anderson

Team Logo

Here


15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here



Requirement Number





CCG 11




CCG 23


CCG 43


CCG 45




Team Logo

Here

(If You Want)



Trade amp Selection






bull Non rigid wing




bull Rigid wing




Team Logo

Here

(If You Want)




Team Logo

Here





2 Check payload




bull Data Reduction


outliers

2 Extract outliers


-Plot with outliers

Team Logo

Here


11



the wings







Team Logo

Here

(If You Want)

12



Hinged Wings

Deployed

Circuit Board

Tail Boom

Fuselage

Vertical

Stabilizer

Horizontal

Stabilizer

Launch

Configuration

Battery Pack



Launch

Configuration

Post Deployment

Pitot Tube

Team Logo

Here






be conducted



deployment







Container

13 13

125 mm

310 mm

118 mm

280 mm

Team Logo

Here

(If You Want)

Team Logo

Here



Melissa Anderson

Team Logo

Here


15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Trade amp Selection






bull Non rigid wing




bull Rigid wing




Team Logo

Here

(If You Want)




Team Logo

Here





2 Check payload




bull Data Reduction


outliers

2 Extract outliers


-Plot with outliers

Team Logo

Here


11



the wings







Team Logo

Here

(If You Want)

12



Hinged Wings

Deployed

Circuit Board

Tail Boom

Fuselage

Vertical

Stabilizer

Horizontal

Stabilizer

Launch

Configuration

Battery Pack



Launch

Configuration

Post Deployment

Pitot Tube

Team Logo

Here






be conducted



deployment







Container

13 13

125 mm

310 mm

118 mm

280 mm

Team Logo

Here

(If You Want)

Team Logo

Here



Melissa Anderson

Team Logo

Here


15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)




Team Logo

Here





2 Check payload




bull Data Reduction


outliers

2 Extract outliers


-Plot with outliers

Team Logo

Here


11



the wings







Team Logo

Here

(If You Want)

12



Hinged Wings

Deployed

Circuit Board

Tail Boom

Fuselage

Vertical

Stabilizer

Horizontal

Stabilizer

Launch

Configuration

Battery Pack



Launch

Configuration

Post Deployment

Pitot Tube

Team Logo

Here






be conducted



deployment







Container

13 13

125 mm

310 mm

118 mm

280 mm

Team Logo

Here

(If You Want)

Team Logo

Here



Melissa Anderson

Team Logo

Here


15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here





2 Check payload




bull Data Reduction


outliers

2 Extract outliers


-Plot with outliers

Team Logo

Here


11



the wings







Team Logo

Here

(If You Want)

12



Hinged Wings

Deployed

Circuit Board

Tail Boom

Fuselage

Vertical

Stabilizer

Horizontal

Stabilizer

Launch

Configuration

Battery Pack



Launch

Configuration

Post Deployment

Pitot Tube

Team Logo

Here






be conducted



deployment







Container

13 13

125 mm

310 mm

118 mm

280 mm

Team Logo

Here

(If You Want)

Team Logo

Here



Melissa Anderson

Team Logo

Here


15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here


11



the wings







Team Logo

Here

(If You Want)

12



Hinged Wings

Deployed

Circuit Board

Tail Boom

Fuselage

Vertical

Stabilizer

Horizontal

Stabilizer

Launch

Configuration

Battery Pack



Launch

Configuration

Post Deployment

Pitot Tube

Team Logo

Here






be conducted



deployment







Container

13 13

125 mm

310 mm

118 mm

280 mm

Team Logo

Here

(If You Want)

Team Logo

Here



Melissa Anderson

Team Logo

Here


15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

12



Hinged Wings

Deployed

Circuit Board

Tail Boom

Fuselage

Vertical

Stabilizer

Horizontal

Stabilizer

Launch

Configuration

Battery Pack



Launch

Configuration

Post Deployment

Pitot Tube

Team Logo

Here






be conducted



deployment







Container

13 13

125 mm

310 mm

118 mm

280 mm

Team Logo

Here

(If You Want)

Team Logo

Here



Melissa Anderson

Team Logo

Here


15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here






be conducted



deployment







Container

13 13

125 mm

310 mm

118 mm

280 mm

Team Logo

Here

(If You Want)

Team Logo

Here



Melissa Anderson

Team Logo

Here


15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

Team Logo

Here



Melissa Anderson

Team Logo

Here


15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

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EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











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Overview







drops to 55C




as expected





Team Logo

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Overview


Integration




Design PCB


Develop FSW







Team Logo

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(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

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Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

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(If You Want)

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Management

Melissa Anderson

Team Logo

Here

(If You Want)

















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Total $29080

10 Margin $2980

Total $31988

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(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

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Program Schedule


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Conclusions





chosen






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15


GPS Payload M10382






airspeed




Micro Camera




ADC in MCU



supplied


Team Logo

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(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)




Requirement Number



CCG 21




CCG 45










Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)




ndash Ublox 6 chip



options




bull 66 channels



$1515







$1934

Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


Air Pressure Sensor

Trade amp Selection

Choice MS5611



ndash Best accuracy





measurement

bull SPI interface



$1442


bull Simple solder

connection


measurement


bull I2C interface


$1062


measurement

bull +- 1 kPa

bull I2C interface


$598

Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here





19

Pitot Tube


Homemade Pitot tube

using MS5611

Pressure sensors


measure altitude




$ 35 - Estimated

HK Pilot Digital

Airspeed and Pitot

tube set






could be found

bull I2C interface

$4944




length

$6304


Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Trade amp Selection


‒ Experience


‒ Best accuracy




bull Experience

bull Thermistor

bull +- 0005-0015degC

accuracy


3

$039


bull Thermistor



sheet


$170




bull Surface Mount

$283

Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)










enhancement

bull Easy access to


bull Heavy $1500


Camera

bull Experience

bull Light weight


of memory through a

micro SD



bull Light weight


Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

Team Logo

Here

23


Will Barton


Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here





Container


Container


pattern

gt400m

400 +-10 m

lt 400m 400-0 m

Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here


25





CCG 11






CCG 3



CCG 4



CanSat

CCG 7





Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


Trade and Selection








Descent Control

Mechanism Pros Cons


Spill Hole







Hole







than parachute




Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


Selection and Trade


System Pros Cons

Symmetric airfoil

(NACA 0012)

Simple model


LD 2deg of 76

Cambered airfoil

(NACA 2410)

LD 2deg of 107

Stall AoA 9deg









Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here




size parasheet

119863 =1

21205881199072(119860119888119862119889 119888119900119899119905119886119894119899119890119903 + 119860119901119862119889 119901119886119903119886119904ℎ119890119890119905)




of the radius

bull 119860119901 = 0991205871199031199012


yields

119903119901 = 2119898119892minus1205881199072119860119888119862119889 119888119900119899119905119894119886119899119890119903

991205871205881199072119862119889 119901119886119903119886119888ℎ119906119905119890

Variable Name Input

119862119889 119888119900119899119905119886119894119899119890119903 Coefficient of

Drag of

Container

085

119862119889 119901119886119903119886119904ℎ119890119890119905 Coefficient of

Drag of

Parasheet

08



120588 Density of air 1225 1198961198921198982

119898 Mass

5 kg w

payload 15 kg

wo payload

119892 Gravity 9811198981199042


Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


(cont)



previous slide




Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here



bull119867 = 119867119879119900119865



119914119949119914119941


bull 119881infin =119867

sin 120579


bull119878 =119882

1

2120588119867

1198621198892

1198621198973


bull119888 = 119878119887



2

119892119877

30


H Height 400 m

ToF Time of

flight 120 s

ρ Density 1225

Kgm3

g Gravity 981 ms2

W weight 350 N

Cl Lift

Coefficient 02908

Cd Drag

Coefficient 002718

b Wing Span 30 cm

R Circular

Radius 250 m


Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here



bull Vertical speed


bull 120579 = 534deg

bull Airspeed

bull 119881infin= 3582 119898119904

bull Wing Area

bull 119878 = 15156 1198881198982

bull Cord Length

bull 119888 = 32 cm

bull Bank Angle

bullΦ = 2762deg

bull Aspect Ratio

bull119860119877 = 594



released at 400m

Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

Team Logo

Here



Will Barton

Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here









ndashNo lasers

bull Container







Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Requirements






CCG 11






CCG 3



CCG 4






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


Trade amp Selection








bull Fiberglass

bull Wood


Wing Spar bull Wood

bull Carbon Fiber

bull ABS


strength of carbon

fiber More modular

than ABS


bull ABS


more interior room

Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Trade amp Selection


System Pros Cons






bull Limited Range

bull Higher weight

Mechanical linkage

Direct Drive pivot




Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here



Payload Materials













Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here


Container Materials



ndashRF transparent









Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here










use of a servo


prevent jostling

Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here




standoffs and bolts









using hot glue

bull Requirements


shock ndash CCG 16



bull DCS


pins


Kevlar cord



DCS


Kevlar Cord

(Container)

bull Easy to

work with

bull Strong

bull Larger by

volume

Monofilament

Fishing Line

(Container)


with

Metal hinge pin

(Payload)

bull Easier to

manufacture

bull Easy to

remove

bull Heavy

Built in pivots

(Payload)


manufacture

Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


Mass Budget


Container

Part Mass Method

Sides 93 g Modeled



Margin (10) 15 g

Total 168 g

Payload

Part Mass Method



Boom 16 g Estimated

Tail 20 g Estimated


Margin (20) 54g


Total Mass = 494g




Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

Team Logo

Here




Nate Roth

Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


CDH Overview

Presenter Nate Roth




commands

MCU ATXMEGA128A4U





processing

Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


CDH Requirements

Presenter Nate Roth




CCRG 21




CCRG 23






CCRG 44




CCRG 24



Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Trade amp Selection


(KB)

IO

Pins

SRAM

(KB)

Hardware

Modules

Max CPU

Frequency

(MHz)

Max ADC

Sampling

Rate

(ksps)

Pin

Count

Atmel AT32UC3A3128 128 110 64

USARTx4

SPIx2 USBx1

ADCx1

66 533 144


USARTx5

SPIx2 USBx1

ADCx1

32 250 44

Atmel ATUC256L3U-

AUT-ND 256 51 32

USARTx4

SPIx1 ADCx1

USBx1

50 460 48




‒ Internal RTC


Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)






Adesto AT25SF041-


Micron M25PE80-


Panasonic RP-




‒ Small size


Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here





External NXP 32 I2C

Variable frequency

setting


Choice Built In


Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)






Presenter Nate Roth



900 MHz Mad

Mushroom



900MHz Duck

Antenna


900MHz Duck

Antenna

Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


Radio Configuration

Presenter Nate Roth










phases


Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here




















Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)




format










Presenter Nate Roth

Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

Team Logo

Here



Design

Jarod Matlock

Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


EPS Overview



ndashPower source

bull Xbee Pro 900


bull MS5611 Sensor


temperature



source to system

bull Thermistor



bull Camera


bull GPS


bull Switch


through hole

Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


Microcontroller

Pitot Tube

3V Batteries

Regulator

Buzzer

Switch

Cutoff

Device

Mosfet

Ground

Radio

Legend

Power line

Camera

LEDs

Exposed Components

Thermistor

Regulator

EPS Overview (cont)

Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here


55


Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


EPS Requirements





adhesives

CCG 17


second

CCG 21





CCG 39




approved before use

CCG 42



CCG 45


Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)




Microcontroller

PT Sensor

(2)

Surefire 3V

Batteries in

series (2)

33 V

Regulator

Buzzer

Switch

Nichrome

wire

N-

Channel

Mosfet

Ground

Radio

Legend

Data Signal

Power line

Camera

LEDs

Exposed Components

Thermistor

42 V

Regulator

Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here



Model Pros Cons


Battery)


bull High amperage



mishandled


(Ni-MH)







temperatures





Concerns)




ndashHigh amperage

Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


Power Budget



MS5611 PT


808 16 Mobius


XBEE Radio


XBEE Radio


Atmel

AT32UC3A0128-

ALUR



Total 58265 mA

Margin

1400 119898119860ℎlowast

58265 119898119860= 24 ℎ119900119906119903119904


Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Trade amp Selection







package

bull I2C



$156


time


bull SPI

bull 8 pin SOT3

package


$189


on MCU

bull Direct

communication



time

~$100

-MCU

Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


FSW Overview



driver files



CanSat





and voltage






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


FSW Requirements





CCG 21




CCG 23




processor resets

CCG 37



commands received

CCG 44

Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)




POWER ON

Measure ground

altitude pressure

and GPS location

Begin mission

time and packet

count increment

Send ldquoready to


PRE LAUNCH

Begin transmitting

data at 1 Hz

Collect data

Begin real time

plotting

Altitude

increases

more than

10 meters

ASCENT

Send data at 1 Hz

Collect data

Continue real time

plotting

Previous

altitude is

greater than

new altitude

Receive test

command

CONTAINER DESCENT

Send data

Collect data


Altitude is

400 meters

or less

GLIDER DESCENT



Send data at 1 Hz

Collect data



Last 5 altitude

readings were +-

1 m of each other

LANDED

Turn on buzzer

Stop transmitting

Complete real time

plotting

Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here


FSW recovery




ndashData saved

bullFlight state

bullTemperature

bullPressure

bullAltitude

bullVelocity



Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)














wait 5 seconds


Glider FSW Plan

Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)






Assemble electrical



code




testing on rocket

launches

Set synchronous




functional flight


the first physical





and radio








Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

Team Logo

Here



Beth Dutour

Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


GCS Overview


Payload

XBEE Pro on

payload

Payload

antenna


GCS Laptop

900 MHz

transmission

MHFII

RP-SMA

Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here


70








CCG 34



CCG 35


Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here



Antenna Pros Cons


Antenna



antennas

bull 629 cm long


of the payload




polarization


Laird PC906N Yagi


antenna




‒ Experience

Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)


(cont)













Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here





file




improve readability



Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here



Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

Team Logo

Here



Nathan Endres

Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Mechanical Testing

















Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Overview

Subsystem Testing

Electronics Testing






ndash Breadboard


bull XBEE tests



FSW tests




Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Overview




container






damage


functional test


Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Overview











Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Overview







drops to 55C




as expected





Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Overview


Integration




Design PCB


Develop FSW







Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

Team Logo

Here



Eliza Dellert

Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Events




CanSat crew


GS team

Fit check

CanSat crew

Weight check

CanSat crew


GS team


communication

GS team

Assemble CanSat

CanSat crew


CanSat crew


pad

CanSat crew




operations


GS team

Recover payload

Recovery officer

Turn in telemetry

GS team

Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Events (cont)


Team Members

bull CanSat crew

ndash Eliza Dellert

ndash Will Barton

ndash Jarod Matlock

ndash Lloyd Walker

bull GS team

ndash Nate Roth

ndash Beth Dutour

ndash Nathan Endres




Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)



Events (cont)




and Excel



transmission




bull Fit check





with GS)

Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)





ndash Content


bull Checklists



ndashAntenna setup




ndashLaunch







Development Plan

86

Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)











CanSat 2016 SkyDive


Contact spaceuahedu



Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

Team Logo

Here



Lloyd Walker

Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here




deployment



Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes





Comply

13

3





Comply

13



4




Comply

26



Comply

13



parts of the CanSat

Comply

13


operations

Comply

13


payload section

Comply

13


10 m

Comply

9

11




Comply




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes






Comply

40








20




Comply 40




23





Comply 51




Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


number Comply 49



toward the ground

Comply

36


in color Comply 22








34



held antenna

Comply 69

35




Comply 69



37




Comply 50


Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here



Rqmt

Num Requirement

Comply No

Comply

Partial

X-Ref Slide(s)

Demonstrating

Compliance

Team Comments

or Notes


39




Comply 55


glider

Comply

4055








45



GPS speed

Comply 19


47



fails

Comply 64


location Comply 55




Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

Team Logo

Here


Management

Melissa Anderson

Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)

















Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

Team Logo

Here

(If You Want)


Program Schedule


Team Logo

Here

(If You Want)




Team Logo

Here

(If You Want)


Conclusions





chosen






Team Logo

Here

(If You Want)











Total $29080

10 Margin $2980

Total $31988

Team Logo

Here

(If You Want)








Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

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Program Schedule


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Conclusions





chosen






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Antenna

$3895 - Actual





Income Grant $7365

Hardware $31988

Other $5847

Total Costs $559745

$7365-$559745= $17675 under budget

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Program Schedule


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Conclusions





chosen






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Program Schedule


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Conclusions





chosen






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Conclusions





chosen






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Conclusions





chosen






Documents

University of Alabama, Huntsville PDR