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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.
thierry.tin-hin@airbus.com
ADS-B Reminders
Complete Range of AIRBUS ADS B SolutionsComplete Range of AIRBUS ADS-B Solutions
AIRBUS Customer Support
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
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
September 2011AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN
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
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
•Wake vortex category
•Etc.Page 4
ADS-B Applications
September 2011AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN
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
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
ADS B APT: Airport surfaces ATSA SURF: Airport Surfaces
Page 5
ATSAW AIRB – Airborne
September 2011AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN
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)
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Page 6
ATSAW ITP – In Trail Procedure
September 2011AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN
Flight number Wake Vortex categoryFlight number
Aircraft orientation (track)
GPS position
Wake Vortex category
Ground speed
Relative altitude and vertical 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
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
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).
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Page 8
September 2011
Reminders on ICAO Separation Standards
AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN
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
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Page 9
September 2011
Flight Level Change with new ITP Procedures
AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN
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.
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Page 10
ATSAW VSA – Visual Separation on Approach
September 2011AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN
p pp
Flight number Wake Vortex categoryFlight number
Aircraft orientation (track)
GPS position
Wake Vortex category
Ground speed
Relative altitude and vertical 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
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Page 11
ADS-B Reminders
Complete Range of AIRBUS ADS B SolutionsComplete Range of AIRBUS ADS-B Solutions
ADS-B Reminders
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
AIRBUS ADS-B Roadmap
September 2011AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN
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
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Separation R&TR&T
Page 13
ADS-B RAD: DO 260B Impacts
September 2011AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN
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.
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
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
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Additional TextAdditional Text InformationInformationPage 15
September 2011AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN
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
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Page 16
ATSAW in A350 Cockpit
AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN September 2011
pSame Same SymbologySymbology
Commonality with A320/A330/A340 operating principles
Additional TextAdditional Text InformationInformation
InteractionInteraction MeansMeans A350 Cockpit interactivity
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
InteractionInteraction MeansMeans A350 Cockpit interactivity=
More efficient workflowPage 17
ATSAW Display Samples
AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN September 2011
p y p
Better identification of trafficBetter understanding of traffic environmentImproved flight efficiencyp g y
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Page 18
ATSAW Display Samples
AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN September 2011
p y p
ATSA AIRB ATSA SURF
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Page 19
Avionics Architecture
AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN September 2011
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
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
* 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
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
The AIRBUS Support for our Customers
September 2011AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN
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
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Page 22
Summary 1/2
September 2011AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN
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
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Page 23
Summary 2/2
AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN September 2011
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
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
hardware changeshardware changesPage 24
AIRBUS Solutions and Roadmap - ADS-B OUT & ADS-B IN September 2011
• 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.
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Page 25
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