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ADS-B Out, In and GNSS Requirements Update. Europe Link 2000+ 2011- 2015. CASCADE Pioneer Phase – 2008 DO 260 (AMC 20-24). US Capstone Project Alaska. Canada Hudson Bay November 2010. Europe TCAS Change 7.1 2012 - 2015. Single European Sky - DO 260B Mandate 2015 -2017. - PowerPoint PPT Presentation
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© 2010 Rockwell Collins, Inc. All rights reserved.
ADS-B Out, In and GNSS Requirements Update
NRA
ITP
ITP
ITP
Australia ADS-B outRule 2008
Mandate 2013
ChinaADS-B Out NRA Trials
Atlantic OceanATSA – ITPFAA GATI
Single European Sky - DO 260B
Mandate 2015 -2017JapanR&D
Asia/Pacific ICAOADS-B Implementation
Task ForceGround infrastructure andprocedures development
US Capstone ProjectAlaska
Pacific OceanATSA-ITPFAA GATI
Canada Hudson Bay November
2010US ADS-B-out DO 260B
Mandate 2020
Pacific OceanATSA-ITPFAA GATI
Europe TCASChange 7.12012 - 2015
Europe Link 2000+ 2011- 2015
CASCADE Pioneer Phase – 2008
DO 260 (AMC 20-24)
US ADS-B-out Infrastructure 2013
UPS/ACSSSafeRoute
2008 Certified
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
Presentation Outline
• Overview
• ADS-B Out
• ADS-B In
• ADS-B In and GNSS Requirements
2
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
Mandate Summary (DO 260B)
• Europe - Forward Fit Mandate January 2015– Retrofit Mandate now February 2017 or 2018
• 1 or 2 year slip
• Australia Upper Airspace (DO 260 )– Voluntary, though separation services being provided today– December 2013 Upper Air Space Mandate
• SA Aware GPS Sensors will be required• For forward fit only
• Canada Hudson Bay & areas with limited SSR coverage (DO 260)– November 2010 Exclusionary Airspace
• 5 NM separation services being offered– No plans for a 260B mandate
• US DO 260B mandated by 2020• No FF to RF segmentation – 100% equipped rule
ANSP readiness(ground systems and integration) isthe core issue!
3
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
GPS Requirements for DO 260B Mandate• Europe
– The European Rule asks for (E)TSO-129A as a minimum– SA=ON is acceptable
• Though SA=OFF (Aware) is preferred
• Canada– SA=ON is acceptable
• Though SA=OFF (Aware) is preferred
• United States– A GPS receiver that is SA Aware will be necessary
• FAA requirement is for a NACp of 8• 100% availability along enroute will determine GPS requirements
• The quick summary of SA=Off/AWARE or SA=ON– Australian rule will require SA Aware for forward fit (2017)– FAA rule will require SA Aware at a minimum– Europe recommends SA aware (doesn’t require)– Canada recommends SA aware (doesn’t require)
Though not stated!Likely will require GPSWith WAAS. A readingof AC 90-ADS-B isrequired?
4
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
ADS-B
Current Surveillance EnvironmentSecondary Surveillance Radar ADS-B Out
ADS-B InApplications
ADS-B In
• Receive • Merge TCAS & ADS-B Targets
• Surface Ops • In Trail Climb Procedures
• Visual Separation on Approach
• Sequencing & Merging
• Etc.
Altitude4096 CodeACFT Addr
PositionVelocityFlt ID, etc
Flight IDSurveillance ID
EnhancedMode S
ElementaryMode S
ExtendedSquitter
Mode A /CMode S
Selected AltMach NoMag HdgRoll AngleTrack AngleTrack Angle Rate
TASIASGSVS
TransponderTCAS /
Traffic Computer
DO260or
DO260B
ISS-2100, TPR-901TSS-4100, TDR-94D
GLU-920 or GLU-925GPS-4000S ISS-2100, TTR-2100
TSS-4100, TTR-4100
SA=OFFGPS Sensor
5
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
ARINC 718A-3/4 Update - An indication of the changes• The development of DO-260B has required additional changes and
more inputs into the transponder– GPS Antenna Position to support POA
• Requires about 32 states for ~ 2 meter accuracy– Other installation related issues are being addressed in the A718-4 work
Current 718A-2 Program Pin Utilization
Minor changes are being incorporated in 718A-4 6
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
Some Pretty Pictures
7
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
ADS-B Out
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
TDR-94D Transponder – Design FeaturesFunctionality• Elementary and Enhanced Surveillance
Compliant – RTCA DO-181C
• ADS-B Extended Squitter • DO-260A Change 2A
Hardware• RTCA DO-160D Compliant
Software• DO-178B Level B Software Design
TDR-94D
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
TPR-901 - Federated Transponder • 822-1338-021 (Airbus) 822-1338-003 (Boeing)
– Elementary Surveillance & Enhanced Surveillance– ADS-B Out DO-260 (Extended Squitter)– DO-181C and JTSO 2C112b – Interface standard ARINC 718A or 718-4 – DO-160D
• 822-1338-004 (B747-8 Only)– Elementary Surveillance & Enhanced Surveillance– ADS-B Out DO-260A Change 2 (Extended Squitter)– TSO C166– Updated to DO-181D (ED-73C) and TSO C112c (ETSO C112c)– DO-160D
• 822-1338-225 (Airbus) and -205 (Boeing)– Elementary Surveillance & Enhanced Surveillance– ADS-B Out DO260B – TSO C166b– DO-181E (ED-73C) and TSO C112d (ETSO C112c)– Interface standard 718A-4– DO-160G
DO 260B Development Underway. Certification planned for 3rd Qtr 2013
For Boeing aircraft SB 503 creates more robust filtering to eliminate position jumping issue. It converts a -003 to a -005.
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
• Business and Regional Aircraft
• Air Transport Aircraft
Integrated Transponder
ISS-2100 -8 MCUTCAS function/Traffic ComputerTransponder, Weather Radar and Terrain Warning functions
DO260-B 4th Quarter 2013
11
TSS-4100 -4 MCUTCAS, Traffic Computer, XPDR
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
ADS-B In (Traffic Computer)
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Next Generation TCAS and Traffic Computer Product Line Developments– TTR-2100 is Plug and Play with the TTR-921– All products are Traffic Computer Capable– Using a common traffic computer architecture– Product line ADS-B In applications development
• Though will require display customization for each aircraft type
TCAS with Traffic Computer Summary
ISS-2100 -8 MCUTCAS function/Traffic ComputerTransponder, Weather Radar and Terrain Warning functions
TTR-2100 -6 MCUFederated TCAS IITraffic Computer
Boeing 787/C 919
Airbus/Boeing in Production Aircraft
Business, Regional & Helicopter aircraft
Common Traffic
Computer and
Traffic Apps.
Common Traffic Computer Design enables re-use of ADS-B In Applications13
TSS-4100 -4 MCUTCAS, Traffic Computer, XPDR
TTR-4100 -4 MCUTCAS, Traffic Computer,
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
TTR-921 versus TTR-2100 Physical Changes
TTR-2100 Front ViewTTR-921 Front View
14
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
15
Fusion Symbology Evaluation
The Complexity and Difficulty of Displaying
Aircraft Targets
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
16
Fusion Symbology Evaluation
Selected-No Flight ID-Data Block Displayed
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
17
Fusion - TCAS RA Event
Focus on TCAS event -Minimize ADS-B Information
TA Symbol with directionality
RA Symbol with directionality -TBD/Under study
Fusion Symbology Evaluation
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
18
Airport Surface with Traffic
Data Block
Selected Aircraft
ANZ139Range: 3NMSpeed: 150KTS
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
GNSS Requirements
© Copyright 2011 Rockwell Collins, Inc. All rights reserved.
• Current GLU-925 (SA = Aware)• ILS (Category IIIB)• Compliant with DO-229D (without SBAS)
– TSO 145A without SBAS• Provides NIC ≥ 7 (99.9% availability)• Accommodates Category I GLS
• GLS Category I Certified on Airbus & Boeing aircraft• Supports SIL = 3 for ADS-B Out
• System Integrity Limit• FLS (FMS Landing System) Capability
• Airbus platforms only• Current GLU-920 (SA = On)
– ILS (Cat IIIB)– Compliant with TSO-C129A
• SA=On– SA=Off Service Bulletin available today (Boeing)
• Compliant with TSO-C129A• Will provide NIC ≥ 7 (99.9% availability)• Will not accommodate SBAS, GLS, or Galileo
• Upgrade of GLU-920 to GLU-925– SB 503 converts 920 to GLS 925 (Boeing)– SB 504 converts 920 to Non-GLS 925 (Boeing)– SB 505 converts the 920 to SA=Off (Aware)
GLU Status
GLS = GNSS Landing SystemGLU = GNSS Landing UnitSA = Selective AvailabilitySB = Service BulletinTSO = Technical Standard Order
20
A350 Will Integrate SBAS (WAAS) Capability into the MMR