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ADS-B Out, In and GNSS Requirements Update

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.

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ADS-B Out, In and GNSS Requirements Update

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  1. 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 TCASChange 7.12012 - 2015 Single European Sky - DO 260B Mandate 2015 -2017 US ADS-B-out DO 260B Mandate 2020 NRA Atlantic Ocean ATSA – ITP FAA GATI China ADS-B Out NRA Trials Japan R&D UPS/ACSS SafeRoute2008 Certified ITP US ADS-B-out Infrastructure 2013 Pacific Ocean ATSA-ITP FAA GATI ITP Asia/Pacific ICAO ADS-B Implementation Task Force Ground infrastructure andprocedures development ITP Pacific Ocean ATSA-ITP FAA GATI Australia ADS-B out Rule 2008 Mandate 2013

  2. Presentation Outline • Overview • ADS-B Out • ADS-B In • ADS-B In and GNSS Requirements

  3. Mandate Summary (DO 260B) ANSP readiness(ground systems and integration) isthe core issue! • 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

  4. 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 GPS With WAAS. A readingof AC 90-ADS-B isrequired?

  5. Transponder TCAS / Traffic Computer ADS-B Current Surveillance EnvironmentSecondary Surveillance Radar ADS-B Out ADS-B In ADS-B In Applications Mode A Enhanced Elementary Extended / C Squitter Mode S Mode S Mode S • Receive • Merge TCAS & ADS-B Targets • Surface Ops • In Trail Climb Procedures • Visual Separation on Approach • Sequencing & Merging • Etc. Selected Alt Altitude TAS Position Flight ID Surveillance ID 4096 Code Velocity Mach No IAS ACFT Addr Mag Hdg GS Flt ID, etc DO260 or DO260B Roll Angle VS Track Angle Track Angle Rate SA=OFF GPS Sensor ISS-2100, TPR-901 TSS-4100, TDR-94D GLU-920 or GLU-925 GPS-4000S ISS-2100, TTR-2100TSS-4100, TTR-4100 5

  6. 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

  7. Some Pretty Pictures

  8. ADS-B Out

  9. TDR-94D Transponder – Design Features Functionality • 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

  10. TPR-901 - Federated Transponder For Boeing aircraft SB 503 creates more robust filtering to eliminate position jumping issue. It converts a -003 to a -005. • 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 3rdQtr 2013

  11. Integrated Transponder • Business and Regional Aircraft • Air Transport Aircraft TSS-4100-4 MCU TCAS, Traffic Computer, XPDR ISS-2100 -8 MCUTCAS function/Traffic ComputerTransponder, Weather Radar and Terrain Warning functions DO260-B 4th Quarter 2013 11

  12. ADS-B In (Traffic Computer)

  13. TCAS with Traffic Computer Summary 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 TSS-4100-4 MCU TCAS, Traffic Computer, XPDR Common Traffic Computer and Traffic Apps. Business, Regional & Helicopter aircraft TTR-4100-4 MCU TCAS, Traffic Computer, TTR-2100-6 MCU Federated TCAS II Traffic Computer Airbus/Boeing in Production Aircraft ISS-2100 -8 MCUTCAS function/Traffic ComputerTransponder, Weather Radar and Terrain Warning functions Boeing 787/C 919 Common Traffic Computer Design enables re-use of ADS-B In Applications 13

  14. TTR-921 versus TTR-2100 Physical Changes TTR-921 Front View TTR-2100 Front View

  15. Fusion Symbology Evaluation The Complexity and Difficulty of Displaying Aircraft Targets

  16. Fusion Symbology Evaluation Selected-No Flight ID-Data Block Displayed

  17. TA Symbol with directionality RA Symbol with directionality -TBD/Under study Fusion Symbology Evaluation Fusion - TCAS RA Event Focus on TCAS event -Minimize ADS-B Information

  18. Selected Aircraft Data Block Airport Surface with Traffic ANZ139 Range: 3NM Speed: 150KTS

  19. GNSS Requirements

  20. GLU Status • 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) GLS = GNSS Landing SystemGLU = GNSS Landing UnitSA = Selective AvailabilitySB = Service BulletinTSO = Technical Standard Order A350 Will Integrate SBAS (WAAS) Capability into the MMR

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