PLATFORM | PILOTMichael Kincel - 06219322
2
Airframe Power System
Electronics Mounting System
Platform
3
HLO-1 Platform
SR-B-01
Manual RC
Control
Perform RC Test Flight
SR-D-01400
Gram Payload
Develop Suitable Airframe
SR-D-02Maintenan
ce Document
4
Airframe Power System
Electronics Mounting System
Platform
5
Airframe
MikroKopter MK40 Readily Available Lightweight Durabiltiy Fulfils Payload Requirements
6
Power System
Electronics Mounting System
Platform
Airframe
7
Power System
Vin
5V
GND
LF50A
220uF
ESC 1
Vin
GND
5V
LF50A
Vin
5V
GND
LF50A
220uF
ESC 2
Vin
GND
5V
LF50A
Vin
5V
GND
LF50A
220uF
ESC 3
Vin
GND
5V
LF50A
Vin
5V
GND
LF50A
220uF
ESC 4
Vin
GND
5V
LF50A
12V
Vin
GND
Autopilot100uF
8
Electronics Mounting System
Platform
Airframe Power System
9
Electronics
UART1
USB
UART2
FlightComputerUART
PWM
Input Capture
ModeControl
Unit
UART
InertialMeasurement
Unit
USB
ADC0
UART4
UART3
ADC1
ArduinoNano
PWM
RCReceiver
Signal Input
4x ESCs
UART
MagneticCompass
UART
Camera
Analogue Output
UltrasonicAltimeter
Analogue Output
BatteryVoltage
Ground Station/Vicon
WiF
i
10
Acceptance Testing
HLO-1 Platform
SR-B-01
Manual RC
Control
AT-01
SR-D-01400
Gram Payload
AT-11
SR-D-02Maintenan
ce Document
AT-12
11
Lessons Learnt
Scope Use commercial hardware if navigation is
desired Hardware Development
Minimum of two people developing hardware
Devote more time to hardware development
Dedicated project