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The CASCADE Programme General Aviation ADS-B Workshop ADS-B Technical Issues C. Tamvaclis EUROCONTROL Experimental Centre European Organisation for the Safety of Air Navigation

ADS-B Technical Issue

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Page 1: ADS-B Technical Issue

The CASCADE Programme

General Aviation ADS-B Workshop

ADS-B Technical Issues

C. TamvaclisEUROCONTROL Experimental Centre

European Organisation for the Safety of Air Navigation

Page 2: ADS-B Technical Issue

Content

ADS-B system requirements

ADS-B infrastructure

Equipment availability and certification

Safety and Performance issues

Interoperability issues

Equipment developments

Final remarks

Page 3: ADS-B Technical Issue

ADS-B System Requirements

[ADS-B OUT] Aircraft must broadcast at least 2-D position, barometric altitude, and flight identification

with prescribed characteristics specified in aviation standards integrity, latency, accuracy, continuity, availability …

and including position integrity indication

[ADS-B IN] Ground and airborne ADS-B receivers must report targets within prescribed coverage volumes and with adequate update periods

suitable surveillance data processing and display systems are also neededcoverage and update rates are application dependent

Page 4: ADS-B Technical Issue

Air to ground and air to air broadcast datalinkfor global interoperability 1090 MHz Extended Squitter (1090ES)

locally VDL-4 and/or UAT may also be used

minimum aircraft equipageADS-B OUT

1090ES capable Mode S transponderGNSS receiver and baro altimeter

ADS-B IN1090ES receiverCockpit Display of Traffic Information (CDTI)

minimum ground equipageOne or more 1090ES ground receivers [stations][surveillance data processing system]

for tracking and fusion with other surveillance data

situation display

ADS-B Infrastructure

Page 5: ADS-B Technical Issue

1090ES ADS-B OUT System

Mode STransponderGPS

PositionHFOM

(VFOM)HPL

(VPL)Time

Extended Squitter

IdentityPosition

NUCVelocity

BarometricAltimeter

FL

24-bit address

TransponderControl Panel

Callsign SPI-EI

Page 6: ADS-B Technical Issue

1090ES ADS-B IN System

Mode SReceiverGPS

Own PositionHFOM

(VFOM)HPL

(VPL)Time

BarometricAltimeter

FL

24-bit address

CDTI

Ext. Squitter

IdentityPosition

NUC(Velocity)

Page 7: ADS-B Technical Issue

ADS-B Validation Testbed

ATCC simulator

CWPFPPS

Radars

ADS-B GS

Flight plans

Cockpit

ADSP

ADS-B Network

ADS-B reports

AST cat 21

A/C Sim

Trackertracks

AST cat 62

plots

ADS-B reports AST cat 21

TIS-B

Server

Aircraft Traffic Generator

+recording replays

Airborne Tracker

ADS-B Server

TIS-B GS

Link Error Emulator

RMCDE

ACAS

Page 8: ADS-B Technical Issue

All ADS-B system components are commercially availableEquipment and installation need to be certified for ops useAircraft equipment:

Mode S Transponder: 1090ES potentially a software upgrade on newer transponder models, certified to

RTCA MOPS 260/A and FAA TSO C166EUROCAE ED73B/102 and EASA ETSO 2C112b

1090ES Receiver: Few products in the market, standalone or combined with TCAS

RTCA MOPS 260/A and FAA TSO C166

GNSS Receiver: Pre 2003 GPS receivers may not provide integrity signalling. Required certification:

FAA TSO C129a (RAIM), C145/146 (SBAS), C161 (GBAS)

CDTI: Some products in the market but no certification available

Equipment availability and certification

Page 9: ADS-B Technical Issue

Safety and Performance Issues

Requirements under development by the Requirements Focus Group (RFG)

ED-126 will address ADS-B surveillance in non radar airspaces

The current 1090ES system has been designed to meet requirements in the RTCA MASPS [DO-242/A]

therefore current MOPS may need to be updated in the future

Quality of ADS-B installation onboard the aircraft is critical need for reliable indication of position integrity and low latency

CDTI is critical for airborne surveillance applications [ADS-B IN]requirements are not agreed as yet

Need for airborne tracking function?HMI factors and placement in cockpit

Page 10: ADS-B Technical Issue

Interoperability Issues

Multiplicity of 1090ES standards FAA standardizing on DO-260A while existing equipage is mostly DO-260

DO-260A is backwards compatible with DO-260RTCA recently published DO -260/A Change 1

need for features added in RTCA DO-260A has to be clarified [RFG work]

1090 MHz Band availabilityADS-B over 1090ES operates in the same RF Band as SSR, Mode S, and TCAS/ACASinterference could become a problem in Core Europe

ADS-B IN will be affected firstThere are mitigations

SSR upgrade to Mode S, replacement by ADS-B and more sophisticated ADS-B receivers.

Page 11: ADS-B Technical Issue

Equipment Developments

The CASCADE Programme is sponsoring development of airborne and ground equipment needed for its ADS-B validation activities

ADS-B and TIS-B ground station [Thales ATM]ADS-B system Oct 06

TIS-B system April 07Airborne 1090ES ADS-B/TIS-B Receiver [ Selex Communications]

delivery May 07CDTI [Selex Communications/EUROTELEMATIC]

delivery Dec 06Usable for air traffic situation awareness applications

for general and business aviation aircraft

Page 12: ADS-B Technical Issue

Final remarks

ADS-B OUT over 1090ES can be implemented today existing GPS and Mode S aircraft installations may be upgradeable to ADS-B, need for ADS-B equipment and installation airworthiness approval

ADS-B IN lacks CDTI standards and airworthiness certificationAir Traffic Situation Awareness standards in development [RFG]

There are many ADS-B equipment developments targeting General Aviation, for example:

low power and light weight 1090ES systems a “light” transponder standard is in development

integrated systems:1090ES transponder and receiverGPS and CDTI