AIRBUS ADS-B roadmap - Sep 2011 (NXPowerLite) · AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN September 2011 Mainly software Include wiring between GPS1-XPDR and GPS2-XPDR

Presented by

ADS-B OUT and ADS-B INPresented byThierry TIN HINAirline CNS/ATM SupportAIRBUS Customer Services

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

[email protected]

ADS-B Reminders

Complete Range of AIRBUS ADS B SolutionsComplete Range of AIRBUS ADS-B Solutions

AIRBUS Customer Support


Reminders on Surveillance Techniques

September 2011AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN

qDependent

Provided by the aircraftIndependent

Calculated by the ground y

PrimarySurveillancePrimarySurveillance

y g

Non-CollaborativeNo aircraft equipment

ADS ContractADS Contract

RadarRadar

SecondarySecondary

q prequired

CollaborativeADS-Contract

ADS-BroadcastADS-Contract

ADS-Broadcast

ySurveillanceRadar

ySurveillanceRadar

Active aircraft equipment required

o Mode A : SQWK code – 0000 to 7777 (4096 codes)o Mode C : Barometric altitude reportingo Mode S : Selective interrogation – 24-bit address (16 777 216 addresses)

Enhanced Surveillance (EHS) :– Selected altitude

Barometric pressure setting

Elementary Surveillance (ELS) :– 24-bit address

Flight number – Barometric pressure setting– Speeds: GS, TAS, IAS, Mach– Track, Heading– Etc.

– Flight number– Aircraft altitude– RA report– Etc.

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

Page 3

ADS-Broadcast Concept


p

Interrogation 1030 MHz

No action required from flight crew

Ai ft iti Reply1090 MHz

Aircraft position provided by aircraft

Transmission of data ith t li it tiwithout solicitation

ADS-B Data

•GPS position

•Aircraft identification

•Ground speedp

•Vertical speed

•Track

Wake vortex category


•Wake vortex category

•Etc.Page 4

ADS-B Applications


ppADSADS--B INB IN

Surveillance with ADS-BMode S Transponder

ADSADS--B OUTB OUT

Mode S Transponder

TCAS bl f ADSTCAS bl f ADS B INB INADSADS B OUTB OUT

Airborne Traffic Situational Awareness

TCAS capable of ADSTCAS capable of ADS--B INB IN

Airborne Traffic Situational AwarenessDisplay of enriched traffic information

in the cockpit

ATSA AIRB: Airborne operationsATSA ITP: In Trail Procedure

ADS-B NRA: Non Radar areasADS-B RAD: Radar areasADS-B APT: Airport surfaces

ATSA ITP: In Trail ProcedureATSA VSA: Visual Separation on ApproachATSA SURF: Airport Surfaces


ADS B APT: Airport surfaces ATSA SURF: Airport Surfaces

Page 5

ATSAW AIRB – Airborne


Flight number Wake Vortex categoryFlight number

Aircraft orientation (track)

GPS position

Wake Vortex category

Ground speed

Relative altitude and vertical speed

Construction of Traffic Awareness

Visual Acquisition for See-and-Avoidq

Traffic Information Broadcasts by Aircraft (Blind Broadcast)

Assistance to out the window scans Less useless RA at level offAssistance to out-the-window scans

Reduced mental effort for traffic awareness

Less useless RA at level-off

Anticipation of possible maneuvers (FL change) and developing dangerous it ti (t b fi d b ATC)Optimized radio communication for

traffic update

situations (to be confirmed by ATC)

Improved cooperation with ATC (better understanding of ATC instructions)


Page 6

ATSAW ITP – In Trail Procedure




GPS position


Ground speed


Flight level changes on a more frequent basis

In non-radar airspacesp

With longitudinal separations temporarily reduced

Reduced fuel burn by flying the Improved flight safety by avoidingReduced fuel burn by flying the optimum cruise FL

Reduced emissions

Improved flight safety by avoiding turbulent FLs

Increase of airspace capacity by d i ff t ITP i ft lHigher flight efficiency by flying FLs

with more favorable winds

domino effect: an ITP aircraft leaves space to other aircraft


Page 7

September 2011

Flight Level Change with Current Procedures

AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN

g g

Procedural separation

Procedural separation

P d l tiProcedural separation

= Aircraft that wishes to climb = Aircraft that maintains its FL

As per ICAO PANS-ATM, Doc 4444, Chapter 5:

A longitudinal separation must be maintained during the entireA longitudinal separation must be maintained during the entire vertical maneuver (i.e. stages 1, 2 and 3).


Page 8

September 2011

Reminders on ICAO Separation Standards


p

FL380

FL370

10 min80 NM

30 NM50 NM

FL37050 NM30 NM

10 min

80 NM10 min

80 NM50 NM30 NM

FL360

30 NM

Separation methods as per ICAO PANS-ATM, Doc 4444, Chapter 5:

Mach Technique based on Time Mach Technique based on Distance (RNAV) RNAV 10 RNP 4

p p , , p


Page 9

September 2011

Flight Level Change with new ITP Procedures


g g

Procedural separationFlight crews ANDATC controllers must be trained.

ITP criteria

Temporarily Reduced SeparationDown to 10 NM mini.

• For the ITP concept:= Aircraft that wishes to climb = Aircraft that maintains its FL

For the ITP concept:1. Before the ITP maneuver, ITP criteria must be met.2. During an ITP maneuver, the ITP longitudinal separation between

i ft i li daircraft is applied.3. At final FL, procedural separation must exist with aircraft that are already

at that final FL.


Page 10

ATSAW VSA – Visual Separation on Approach


p pp



GPS position


Ground speed


Application of the Visual Separation on Approach

With ATSAW (easier traffic identification)( )

In VMC

Increased airport landing capacity Reduced probability of wake vortexIncreased airport landing capacity thanks to VSA separations shorter than radar ones

R d d fli ht ti th k t th l b l

Reduced probability of wake vortex encounters as ATSAW helps anticipating speed reduction from the preceding aircraftReduced flight time thanks to the global

increase of airport capacity

preceding aircraft

Reduced radio communication


Page 11

ADS-B Reminders

Complete Range of AIRBUS ADS B SolutionsComplete Range of AIRBUS ADS-B Solutions

ADS-B Reminders


AIRBUS ADS-B Roadmap


DO-260 = ICAO Version 0 Extended SquitterDO-260A = ICAO Version 1 ESDO-260B = ICAO Version 2 ESp

ELS/EHS Certification & ADS-B OUT Capacity AvailableAvailable

ADS-B NRADO 260 (certified): A320/A330/A340DO 260A Chg 1 (certified): A380DO 260A Chg 2 (certified): A320/A330/A340

AvailableAvailableCompliant with Compliant with

EASA AMC 20EASA AMC 20--2424g ( )

ADS-B RAD DO 260B (TBD): A320/A330/A340/A380/A350Aligned withAligned with

A320/A330/A340 C tifi d

ADS-B APT TBD

Aligned with Aligned with future mandatesfuture mandates

ATSAW AIRB/VSA/ITPA320/A330/A340: CertifiedA350: Entry into ServiceA380: TBD

AvailableAvailableTrials to start Trials to start soon (3Q2011)soon (3Q2011)

ATSAW SURF Feasibility study in progress

Spacing

Separation

PrototypingPrototyping

R&TR&T


Separation R&TR&T

Page 13

ADS-B RAD: DO 260B Impacts


p

Include wiring between GPS1-XPDR Mainly software gand GPS2-XPDRAvailable on production line since 2003.

Mainly softwareMinor hardware: Provisions for 2nd GPS input.

H d dHardware upgrade reduced to the minimum

FWC software upgrade

Transmission of new parameters (e.g. length & width code, aircraft

)

FWC software upgradeWiring FWC-XPDR.


category).Page 14

ATSAW in A320/A330/A340 Cockpit

AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN September 2011

p

New InteractionNew Interaction MeansMeansNew New SymbologySymbology

New InteractionNew Interaction MeansMeans


Additional TextAdditional Text InformationInformationPage 15


TCAS and ATSAW Symbolsy

OtherOther ProximateProximate TATA RARA TCAS range ~30 NM

ADS B 100 NM

TCAS OnlyTCAS Only

ADS-B range ~100 NM

TCAS + ADSTCAS + ADS--BB

ADSADS--B OnlyB Onlyyy

Highlighted Selected Highlighted & Selected& Selected

Ground Speed (kt)Wake Vortex Category (L/M/H)

Flight IDTrack oriented


Page 16

ATSAW in A350 Cockpit


pSame Same SymbologySymbology

Commonality with A320/A330/A340 operating principles

Additional TextAdditional Text InformationInformation

InteractionInteraction MeansMeans A350 Cockpit interactivity


InteractionInteraction MeansMeans A350 Cockpit interactivity=

More efficient workflowPage 17

ATSAW Display Samples


p y p

Better identification of trafficBetter understanding of traffic environmentImproved flight efficiencyp g y


Page 18

ATSAW Display Samples


p y p

ATSA AIRB ATSA SURF


Page 19

Avionics Architecture


Cockpit

SURV

Cockpit Interfaces

ApplicationsADS-B OUT ATSAW ADS-B OUT ATSAWApplicationsADS B OUT ATSAW ADS B OUT ATSAW

AESSComputerTCAS+XPDR* TCAS+XPDR*

SensorsMode S TCASGPS

RA

Mode S TCASGPS

RA

Mode S Antennas

TCAS Antennas

GPS Mode S Antennas

TCAS Antennas

GPS


* Capable of ADS-B Out + Capable of ATSAWAlso capable of TCAS Chg 7.1

Page 20

Data Link Communication Reminders

Complete Range of AIRBUS FANS SolutionsComplete Range of AIRBUS FANS Solutions

AIRBUS Customer Support


The AIRBUS Support for our Customers


pp

• Support to aircraft definition and retrofit• In-service support

Engineering

• Flight operations expertise• Assistance to EIS and operational approval, in-service support

Flight Operations

• Academic briefingOperations

• AFM, FCOM, MMEL, AMM• Computer Based Training• Computer Based Training• Airworthiness Capability Declaration for ADS-B OUT & ATSAW• Getting to Grips with Surveillance

Documentation


Page 22

Summary 1/2


y

Applications

ADS-B NRA: Non Radar AreasADS B RAD: Radar Areas

ADS-B NRA: Non Radar AreasADS B RAD: Radar Areas

AIRBUS ADS-B OUT

ADS-B RAD: Radar AreasADS-B APT: Airport Surfaces

ADS-B RAD: Radar AreasADS-B APT: Airport Surfaces

ATSA AIRB: AirborneATSA AIRB: Airborne

NRA – DO 260/260 AEASA AMC 20-24 complianton A320/A330/A340/A380

NRA – DO 260/260 AEASA AMC 20-24 complianton A320/A330/A340/A380

AIRBUS ATSAW

AIRB/VSA/ITPAIRB/VSA/ITPATSA AIRB: AirborneATSA ITP: In Trail Procedure

ATSA VSA: Visual Sep.on App.ATSA SURF: Airport Surfaces

ATSA AIRB: AirborneATSA ITP: In Trail Procedure

ATSA VSA: Visual Sep.on App.ATSA SURF: Airport Surfaces

on A320/A330/A340/A380on A320/A330/A340/A380

RAD – DO 260BRAD – DO 260B

AIRB/VSA/ITPwith TCAS capable of Chg 7.1

on A320/A330/A340on A350 at EIS

AIRB/VSA/ITPwith TCAS capable of Chg 7.1

on A320/A330/A340on A350 at EISpp

More Flight EfficiencyMore SafetyLess Fuel Burn

More Flight EfficiencyMore SafetyLess Fuel Burn

To be available on A320/A330/A340/A380/A350

To be available on A320/A330/A340/A380/A350

SURFFeasibility study in progress

SURFFeasibility study in progressLess Fuel Burn

Less EmissionsLess Fuel BurnLess Emissions

Feasibility study in progressFeasibility study in progress


Page 23

Summary 2/2


y

O ti i d Fli htO ti i d Fli htSame operatingSame operating principles acrossprinciples across

Optimized FlightOptimized FlightCrew WorkflowCrew Workflow

Same operatingSame operating principles across principles across A320/A330/A340 and A380/A350A320/A330/A340 and A380/A350

SESARSESAR NextGenNextGenDesignedDesigned to cope with future to cope with future requirements with minimum requirements with minimum

SESAR, SESAR, NextGenNextGenStandard ApplicationsStandard Applications


hardware changeshardware changesPage 24


• AFM: Aircraft Flight Manual

AMM Ai ft M i t

• SESAR: Single European Sky ATM Research• AMM: Aircraft Maintenance

Manual

• FCOM: Flight Crew Operations

ATM Research

• XPDR: Transponder

• FCOM: Flight Crew Operations Manual

• MMEL: Master Minimum Equipment List

• RA: Radio Altimeter

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of AIRBUS S.A.S. No intellectual property rights are granted by thedelivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS S.A.S. This document and its content shall not beused for any purpose other than that for which it is supplied The statements made herein do not constitute an offer They are based on the mentioned assumptions and are expressed in good faith Where the supportingused for any purpose other than that for which it is supplied. The statements made herein do not constitute an offer. They are based on the mentioned assumptions and are expressed in good faith. Where the supportinggrounds for these statements are not shown, AIRBUS S.A.S. will be pleased to explain the basis thereof.AIRBUS, its logo, A300, A310, A318, A319, A320, A321, A330, A340, A350, A380, A400M are registered trademarks.


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Documents

AIRBUS ADS-B roadmap - Sep 2011 (NXPowerLite) · AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN September 2011 Mainly software Include wiring between GPS1-XPDR and GPS2-XPDR