ADS_B_Deep_Dive

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ADS-B

Flight Technical ServicesFebruary 2013


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Honeywell Proprietary

Honeywell.com

C&PS Flight Technical Services 2

C&PS Flight Technical Services

This material was developed by:

C&PS Flight OperationsHoneywell Aerospace

www.honeywelltraining.com

This material was developed by:

Customer & Product Support Flight Technical Services

Honeywell Aerospace

www.honeywelltraining.com

To download this presentation visit:https://www.mygdc.com/new/static/cpsfltops_training.php


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C&PS Flight Technical Services 3

This document and the information disclosed herein are proprietary data of Honeywell International Inc.Neither this document nor the information contained herein shall be reproduced, used, or disclosed to others

without the written authorization of Honeywell International Inc., except for training on recipients equipment.

Notice Freedom Of Information Act (5 USC 552) And Disclosure Of Confidential Information Generally

(18 USC 1905)

This document is being furnished in confidence by Honeywell International Inc. The information disclosed

herein falls within exemption (b) (4) of 5 USC 552 and the prohibitions of 18 USC 1905.

ECCN 7E994; Schedule B Number 8524.31.0070

C&PS Flight Technical Services / Global Data Center

Notice Of Limitations

The information contained herein has been compiled for training purposes only.

Its use shall be limited to such applications. For exclusive use by Honeywell customers.

Not for reproduction or distribution to other avionic manufacturers.

Copyright Notice

Copyright 2012 Honeywell International Inc. All rights reserved. Honeywell is a registered trademark of

Honeywell International Inc. All other marks are owned by their respective companies.

Honeywell International Inc.

C&PS Flight Technical Services

21111 N. 19thAve.

Phoenix, AZ 85027-2708

U.S.A.

Proprietary and Limitations Notice


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AutomaticPeriodically transmits information with nopilot or operator input required

DependentPosition and velocity vector are derived from

the Global Positioning SystemSurveillanceA method of determining position of

aircraft, vehicles, or other assets

Broadcast

Transmitted information available toanyone with the appropriate receiving

equipment

ADS-B What is it?


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What is ADS-B?

Automatic Dependent Surveillance Broadcast

ADS-B Out - Surveillance technology thattransmits GPS based position and other aircraft or

vehicle information

Identification

GPS position

Altitude (Baro & Geometric) Velocity

Quality and Integrity data, etc.

ADS-B In - Transmitted signals can be receivedby other aircraft as well as ground stations

Traffic Situation can be depicted on Aircraft Display butwith much more information than what TCAS provides

Allows new features based on ADS-B data

Spacing & Merging

Airport Surface Management

In-Trail Procedures

VFR like separation in all weather conditions

ATC Providers and Regulatorsare Interested because

Potentially allows them to decommission

expensive SSR Radars

Provides much better quality

surveillance Position Accuracy

Aircraft State and Intent information

Ultimately will allow more aircraft to use

existing airspace with equivalent or

better safety and efficiency

Low Cost Surveillance Technology


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Benefits of ADS-B

Estimated Savings through 2016 in Hudson Bay $158 million in fuel

436,000 metric tons of CO2 emissions


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Countries with ADS-B Projects ASECNA (Senegal, Congo, Niger, Ivory Coast, Chad and Madagascar)

Guinea, Sierra Leone, Liberia

United Arab Emirates

Congo

Ethiopia

Kuwait

Namibia

Saudi Arabia

South Africa

Afghanistan

China

India

Indonesia/Fiji/New Zealand

CONCESNA (Central America)

Trinidad and Tobago

Australia

Japan

Kazakhstan

Korea

Kyrgyzstan

Myanmar

New Caledonia

Philippines

Singapore

Taiwan

Tajikistan

Armenia

Austria

Bulgaria

Canada

Mexico

Czech Republic

Germany

Greece

Norway

Portugal

Russia

Slovakia

Sweden

Turkey

UK

Ukraine

Jamaica

Peru

USA

Hong Kong


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8

Hudson BayADS-B Out

FL 350-400

FAA ADS-B OutForward Fit and Retrofit

AustraliaRetrofit (FL 290+)

EASA ADS-B OutRetrofit

= Preliminary Dates

DO-260 or later

DO-260 or later

DO-260B or later

DO-260B or later

Gulf of MexicoADS-B Out DO-260A or later

= Improved Access (Helo)

= Firm Dates

Hong KongPBN Routes FL290+

EASAForward Fit

AustraliaForward Fit (FL 290+)

DO-260 or later, SA Aware GPS

DO-260B or later

SingaporeRetrofit (FL 290+)

DO-260 or later

DO-260 or DO-260A

Hong KongHKG FIR FL290+

IndonesiaRetrofit (FL 290+)

DO-260 or later

DO-260 or DO-260A

ADS-B Out Timeline



Honeywell.com

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ADS-B Out Mandate/Proposed Rule DetailsHong Kong (CAD):

ADS-B Out for FL 290 to FL410 DO-260 or DO-260A Equipage by 12-DEC-2013 Limited to HKG-Registered aircraft operating on PBN Routes L6642 and M771 in HKG FIR

ADS-B Out for FL 290 to FL410 DO-260 or DO-260A Equipage by 12-DEC-2014 Limited to HKG-Registered aircraft operating in the HKG FIR

Indonesia (DGCA): ADS-B Out for FL 290 and Above DO-260 Equipage by 12-DEC-2013

Singapore (CAAS): ADS-B Out for FL 290 and Above DO-260 Equipage by 12-DEC-2013

Limited to specific Airways in the Singapore FIR

EASA (via EUROCONTROL):

ADS-B Out DO-260B Equipage by 7-Dec-2017Forward fit 8-JAN-2015, Retrofit 7-DEC-2017

Requires DO-260B ADS-B Out on all aircraft with maximum certificated take-off mass

exceeding 5700 kg or having a maximum cruising true airspeed capability > 250 kts

Applicable to all IFR flights operated in Africa-Indian Ocean and European Regions

Possible exemption for aircraft built prior to 1990; they must request exemption from

EASA before 07-Jul-2017



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The Future of ADS-B In Canada

Source: Nav Canada

Canada:

ADS-B Out for Hudson

Bay/Minto Access, FL 350 to 400

DO-260 access benefits began

JAN-2009

Access penalties if no ADS-B by

17-NOV-2011

Must file published routes if notApproved

Considering expanding area

and/or lowering FL



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Canadian ADS-B Deployments



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Changes in the Hudson & Minto Sectors

Effective Nov 17th, 2011 Aircraft that are not registered

with NAV CANADA as eligible to

receive ADS-B Out surveillance

services, when operating

through the Hudson and Minto

Sectors at a flight planned

altitude ranging from FL350 to

FL400 inclusive, will be required

to file flight plans on published

route structures.

A FAA LOA and TransportCanada OpsSpec is required to

operate in this area

http://www.navcanada.ca/ContentDefinitionFiles/Publications/AeronauticalInfoProducts/AIP/Next/PDF/EN/part_5_aic/5aic_eng_2011_31.pdf

AIC 31/11



Honeywell.com

The Future of ADS-B In Australia

5,000

20,000 30,000

10,000

Australia:

SA aware GNSSU or MMR

data source for new aircraft by

28-Jun-2012

New requirements makefitment and operation of

approved ADS-B avionics

equipment mandatory on, and

from, 12 Dec 2013 for all

Australian aircraft operations at,

or above, FL 290

All new IFR aircraft delivered

to Australia after 6 Feb 2014

must have ADS-B out

http://newsroom.airservicesaustralia.com/releases/one-year-to-go-for-mandatory-ads-b-fitment



Honeywell.com

The Future of ADS-B in the USA

Nationwide Coverage by 2013

USA :ADS-B Out for Gulf of

Mexico Access

DO-260A benefits on 1-JAN-

2010

ADS-B Out for Class A, B, C

Airspace DO-260B Equipage

by 1-Jan-2020

Forward fit and retrofit


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ADS-B Airspace in the USA


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ADS-B Airspace in the USA

ADS-B Performance is required in the following airspace:

Class A, B, and C airspace

Class E airspace areas at or above 10,000 feet MSL over the 48

contiguous United States and the District of Columbia, excluding

the airspace at and below 2,500 feet above the surface

Airspace within 30 nautical miles (NM) of certain identified

airports that are among the nations busiest (based on annual

passenger enplanements, annual airport operations count, and

operational complexity) from the surface up to 10,000 feet MSL.

These airports are listed in appendix D to part 91.

Above the ceiling and within the lateral boundaries of a Class B

or Class C airspace area up to 10,000 feet mean sea level (MSL)

Class E airspace over the Gulf of Mexico at and above 3,000 feet

MSL within 12 NM of the coastline of the United States


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USA ADS-B Deployment

440 Operational

ADS-B Receivers

As of 11/30/2012

Enroute Services


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USA ADS-B Deployment

Advisory Services

FIS-B & TIS-B

As of 11/30/2012

Separation & Terminal Services

ADS-R


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Honeywell.com

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UAT or 1090ES Requirements


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FAA UAT & 1090ES Dual Link System

ADS-B Dual Link System UAT for GA (Universal Access Transceiver)

978 MHz

Cheaper installation

Provides Additional Features (TIS, FIS, Graphical WX, etc)

Reduces Congestion on 1090MHZ Mainly USA and below 18,000

Mode-S 1090ES (Extended Squitter)

1090 MHz

Uses existing Mode-S transponderAdds additional information (the ES)

No additional features because 1090 is already congested

Required above 18,000 and Internationally

Can be used below 18,000


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SSR Antenna Array

PSR Antenna Array

Mode A/C XPNDR

Mode S XPNDR

Transponders


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Progression Of Mode-S XPNDR to ADS-B

AltitudeCodeA/C Address

Flight IDSelected ALTMach NumberMag HDHRoll AngleTrack AngleTrack Angle RateTASIASGSVS

PositionVelocityFlight ID

Uses NUCNavigation

UncertaintyCategory

Mode A/CMode-S Elementary &EnhancedSurveillance

(ELS & EHS)

ADS-BDO-260

Broadcast


Uses NIC &NACp

NavigationIntegrityCategory &NavigationAccuracyCategoryfor Position

ADS-BDO-260A

Broadcast


Changedhow NIC,NAC andSIL are set

Length/WidthPower

ADS-BDO-260B

Broadcast


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SA-Aware GPS Requirement


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How Do The Different Formats Communicate ?

Dual Mode ADS-BGround Station

Air Traffic Control

Non ADS-B

1090ES Mode-SUAT


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Air Traffic Control

Non ADS-B

1090ES Mode-SUAT


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Air Traffic Control

Non ADS-B

1090ES Mode-SUAT


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Air Traffic Control

FIS-B

1090ES Mode-SUAT


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FIS-B


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Cockpit Display of Traffic Information CDTI

ADS-B In functions: (Enhanced) Traffic Situation Awareness (TSA)

(Enhanced) Visual Separation on Approach (VSA)

Oceanic In-Trail Procedures (ITP)

Platform for future CDTIAirport Surface Situation Awareness (ASSA)

Cockpit Final Approach and Runway Occupancy

Awareness (FAROA)

CDTI Assisted Visual Separation (CAVS)

Interval Management (IM)

VFR-like Separation in All Weather Conditions or

Electronic Flight Rule (EFR)

DAL10

+10+20

QH13

-10

-20

AF320

+40

Status:

30

UAL23

+20UAL10-20

ITP REQUEST

ITP View

Formulate ITP CLNC

Flt ID: AF320

Alt: FL340

ITP Di stance : 80 nm

Gspd Dif f: 5 kt

Equip: ADSB

TRK 060+040/-040Alt Band:

ITP distance and location may not match plan view ran ge

Plan View

Alt : REL

Display

Settings


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Fully integrated solution

Traffic displayed on the primary field of view

Limited impact (no new equipment)

ADS-B Traffic from Traffic Computeron Navigation display

Traffic Selectors

Additional informationfrom Traffic Computeron MCDU

Courtesy ofCDTI (ATSAW) in A320, A330 & A340


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-20

+10

+09

Traffic

Selector

+01

EZY1845315 M

IBE7274355 M

AFR6512325 M

What is ATSAW?

Airborne Traffic

Situational AwarenessNew Data When Selected:

Aircraft ID

Ground Speed

Wake Vortex Data (AC Wt Category)

ATSAW Applications: ATSA-AIRB: Airborne Traffic Situational

Awareness

ATSA-VSA: Visual Separation on Approach

ATSA-ITP: In-Trail Procedure

ATSA-SURF: Surface Situational Awareness

Graphic Courtesy of Airbus

Certified on Airbus SA & LR

H ll


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ATSAW: Traffic List on MCDU

Graphics Courtesy of Airbus

H ll


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Visual Separation on Approach

Easier for flight crews to acquire and

then to maintain own visual contact

with the preceding aircraft.

Flight crews maintain a more precise

distance from the preceding aircraft

(anticipating speed change).

Potential runway capacity

improvements in Visual

Meteorological Condition (VMC) and

Alternate VMC

ATSAW: VSA Courtesy of

Honeywell com


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ATSAW: ITP

In-Trail Procedure: Enhanced efficiency: Reduced Longitudinal

separation of 15 NM will be

sufficient for a flight level

change (compared to 80

NM today) Significant fuel saving due

to optimum flight level

Enhanced safety:

Better awareness of traffic

situation during flight levelchange procedure.

Graphic Courtesy of Airbus

Honeywell com


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Courtesy of

ATSAW: ITP Traffic List on MCDU

Honeywell com


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Enhanced Traffic Situational Awareness on the Airport Surface Awareness of Traffic situation

Collision risk anticipation

ATSAW: SURF (Future)

Graphics Courtesy of Airbus

Honeywell com


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Joint FAA/UAL/Honeywell Program

Demonstrated operational benefits enabled by the ADS-B In, In Trail Procedures

Honeywell has, integrated, and certified complete ITP avionics capability as installed on United

Airlines 747-400

Avionics system consists of: Honeywell Traffic Computer, TPA-100B with ADS-B In and ITP capability

Honeywell Transponder, TRA-67B with ADS-B Out capability

Goodrich Class 3 EFB running Honeywell ITP display software

United Airlines will operate approximately 12 Honeywell ITP avionics equipped

747-400 aircraft in the South Pacific (SOPAC) route. Successful trials

completed. FAA in final stages of approval.

ADS-B ITP Enabled Climbs

Sub-Optimal Cruise

Optimal

Successful ITP Trials in SOPAC

Honeywell com


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Example ITP Traffic Display EFB Solution

Honeywell.com


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Issues

Implementation vs. Mature Specification (DO-260, DO-260A, DO-260B) Different standards/equipage

Approved Lists

Flight IDs not properly installed/entered

Off lease

Juristiction change

Flight Plans

RMK/ADSB in first field of Flight Plan Block 18

Several Flight Planning services have trouble with this -> ICAO Flight Plan 2012

How do I know if its working ?

Required IFR Transponder Checks

ATC will tell you !

Honeywell.com


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Nav Canada ADS-B Update

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y

Nav Canada ADS-B Update

May 2, 2012 Update

1000 Approved Aircraft

2000 Capable of being approved (based on data received)

Looking at expanding Hudson and Minto areas (flight levels)

Completed new safety assessment

Excellent Reliability

GPS Position Accuracy

Looking at going from an approved list to Not Approved List

Coincident with Flight Plan 2012 that has a specific ADS-B field (Nov 2012)

Honeywell.com


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The Future Worldwide ADS-B

In June 2011 the FAA approved space based provisioning of ADS-Bsurveillance over oceanic and remote areas

Several companies have announced plans

Iridium

New Iridium Next constellation

81 Low Earth Orbit Satellites

Reserving 20% for hosted payloads like ADS-B

Working on agreements with the FAA and other ANSPs

ADS-B Technologies

Globalstar second generation satellites 24 Low Earth Orbit Satellites

Receives and re-transmits back to ground stations (no smarts in satellite)

Nov 2012 Nav Canada signs agreement to invest in Aireon LLC (Iridium Next)

Honeywell.com


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The Future Worldwide ADS-B

Honeywell.com


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ADS-B Out Product Planning

Product Application DO-260 DO-260A DO-260BAESU

(A380)Air Transport -- Available In Process

TRA-67A Air Transport Available --Replace with

TRA-100B

TRA-100B Air Transport - - TSO 3Q13

Epic Regional, HelicopterBusiness Aviation

-- Available TSO 3/2012

Primus IIRegional

Business Aviation-- --

Available

TSO 1/2011

MST-67Regional

Business Aviation-- --

MST-67B

TSO 4Q13

APEX Business AviationGeneral Aviation

-- -- TSO 3Q13

KT-73 General Aviation Available(non-diversity)

-- Planned

MILACAS Military Transport Available - Military unique IFF solution

Honeywell.com


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