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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.

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ADS-B Out, In and GNSS Requirements Update

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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 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


Presentation outline

Presentation Outline

  • Overview

  • ADS-B Out

  • ADS-B In

  • ADS-B In and GNSS Requirements


Mandate summary do 260b

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


Gps requirements for do 260b mandate

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?


Ads b

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


Arinc 718a 3 4 update an indication of the changes

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


Ads b out in and gnss requirements update

Some Pretty Pictures


Ads b out

ADS-B Out


Tdr 94d transponder design features

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


Tpr 901 federated transponder

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


Integrated transponder

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


Ads b in traffic computer

ADS-B In (Traffic Computer)


Tcas with traffic computer summary

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


Ttr 921 versus ttr 2100 physical changes

TTR-921 versus TTR-2100 Physical Changes

TTR-921 Front View

TTR-2100 Front View


Fusion symbology evaluation

Fusion Symbology Evaluation

The Complexity and Difficulty of Displaying Aircraft Targets


Fusion symbology evaluation1

Fusion Symbology Evaluation

Selected-No Flight ID-Data Block Displayed


Fusion tcas ra event

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


Airport surface with traffic

Selected Aircraft

Data Block

Airport Surface with Traffic

ANZ139

Range: 3NM

Speed: 150KTS


Gnss requirements

GNSS Requirements


Ads b out in and gnss requirements update

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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