GBAS FOR ATCO. June 2017

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GBAS FOR ATCO June 2017

Disclaimer This presentation is for information purposes only. It should not be relied on as the sole source of information, and should always be used in the context of other authoritative sources and the relevant regulations. Most Images or graphics are obtained from internet for non-profit making public educational purpose only. Should the owner of the image/graphic found the use of the image/ graphic not appropriate, please inform Mr. Lam via jcclam@cad.gov.hk to remove the image/ graphic from this presentation. 2

CONTENT Review the Basis of GNSS GBAS Operational Overview Advantages of GBAS Info for ATCO Q&A

BASIS OF GNSS - 1 Time Difference The GPS receiver compares the time a signal was transmitted by a satellite with the time it was received. The time difference tells the GPS receiver how far away the satellite is.

BASIS OF GNSS - 2 Velocity x Time = Distance Radio waves travel at the speed of light, roughly 186,000 miles per second (mps)

BASIS OF GNSS - 2 ATOMIC CLOCKS GPS satellites use Atomic Clocks for accuracy, but because of the expense, most GPS receivers do not. Solution: GPS software uses a fourth satellite to provide a cross check in the trilateration process and update the internal clock simultaneously.

BASIS OF GNSS - 3 Satellite navigation system or satellite constellation support GNSS GPS (United States): GPS was the first GNSS system. GPS was launched in the late 1970s by the United States Department of Defense. As of Feb., 2016 there are 32 satellites in the GPS constellation. GLONASS (Russia): GLONASS is operated by the Russian government. The GLONASS constellation is officially completed in 2015 (since 1996) which consists of 24 satellites and provides global coverage. Galileo (European Union): Galileo is a civil GNSS system operated by the European Global Navigation Satellite Systems Agency (GSA). As of December 2016 the system has 18 of 30 satellites in orbit. Galileo started offering Early Operational Capability (EOC) on 15 December 2016 and is expected to reach Full Operational Capability (FOC) in 2019. The complete 30-satellite Galileo system (24 operational and 6 active spares) is expected by 2020. BeiDou (China): BeiDou is the Chinese navigation satellite system. The system will consist of 35 satellites. A regional service became operational in December of 2012. As of 2016, 23 satellites were launched. BeiDou is expected to provide global coverage by end of 2020.

BASIS OF GNSS 4 GNSS ERROR SOURCES Image courtesy of www.novatel.com

BASIS OF GNSS 4 GNSS ERROR SOURCES Contributing Source Error Range Satellite Clocks ±2 m Orbit Errors ±2.5 m Inospheric Delays ±5 m Tropospheric Delays ±0.5 m Receiver Noise ±0.3 m Multipath ±1 m Data courtesy of www.novatel.com

BASIS OF GNSS 5 RESOLVING THE PROBLEM Image courtesy of FAA Satellite Based Augmentation Systems (SBAS) FAA-Wide Area Augmentation System (WAAS); EASA- European Geostationary Navigation Overlay Service (EGNOS); JCAB-MTSAT Satellite Based Augmentation Navigation System (MSAS); India-GPS-Aided GEO Augmented Navigation System (GAGAN); Russia-System for Differential Corrections and Monitoring (SDCM); China- SNAS (Satellite Navigation Augmentation System) Ground Based Augmentation Systems (GBAS) FAA-Local Area Augmentation System (LAAS); ICAO-GBAS Landing System (GLS)

BASIS OF GNSS 5 RESOLVING THE PROBLEM Contributing Source Error Range Satellite Clocks ±2 m Orbit Errors ±2.5 m Inospheric Delays ±5 m Tropospheric Delays ±0.5 m Receiver Noise ±0.3 m Multipath ±1 m Data courtesy of www.novatel.com

GBAS - OPERATIONAL OVERVIEW LAND SECTION Ground Facilities: GPS Reference Receivers (RR) Very High Frequency (VHF) Data Broadcast (VDB) Transmitter Equipment Room ATC Status Display Image courtesy of Honeywell

GBAS - OPERATIONAL OVERVIEW ONBOARD EQUIPMENT SECTION Cockpit Displays 737NG GLS forward fit, retrofit 787 GLS basic 747-8 GLS basic MMR GPS Antenna A-380 GLS Option A-320 GLS option A-340 GLS option A-330 GLS option A-350 GLS Basic Aircraft Surfaces Aircraft Pilot Interface Antenna GPS Differential Corrections, Integrity Status and Approach Coordinates DATALINK VHF Data Broadcast (VDB) DGPS Computes Differential Corrections Provides Integrity Check Provides Approach Coordinates Transmitter Encoder Broadcast Information GPS error corrections, integrity, AND path points Local Ground Facility Autopilot DGPS Differential GPS MMR Multi-Mode Receiver (GPS, VDB, ILS, etc) VDB VHF Data Broadcast (Link to aircraft) Data Broadcast Monitor Receiver Decoder Image courtesy of Honeywell

GBAS - OPERATIONAL OVERVIEW ONBOARD EQUIPMENT SECTION ILS look alike Glideslope Localizer GLS GPS Landing System ILS Instrument Landing System Image courtesy of Honeywell

GBAS - OPERATIONAL OVERVIEW ONBOARD EQUIPMENT SECTION Image courtesy of Airbus

GBAS - OPERATIONAL OVERVIEW ONBOARD EQUIPMENT SECTION Image courtesy of Airbus

ADVANTAGES OF GBAS - GENERAL Increased airport capacity: GBAS unlocks capacity constraints Offers precision approach where ILS cannot due to geography Relatively more flexible design criteria on approach and potentially for departure Eliminates ILS sensitive/ critical area Lower life-cycle cost: GBAS is more cost efficient than ILS For multiple runway, One GBAS system serves all runway ends, initial acquisition cost is lower Lower maintenance cost Lower flight inspection cost Safety: GBAS improves safety Offers precision approach where ILS cannot due to geography Signal stability (immune to signal interference inherent in ILS) Reduced noise/shorter routes: Variable glide slopes, RNAV/RNP to GLS finals Airlines benefit: fuel and emission savings, increased schedule flexibility, avoid noise violations Airports benefit: increased capacity and schedule flexibility, improved community relations

ADVANTAGES OF GBAS - ATC Image courtesy of Honeywell Multiple Concurrent Operations

Image courtesy of FAA INFO FOR ATCO CHART

INFO FOR ATCO-OTHER ISSUES Wake? RWY Marking? Lighting? Spacing? Integration? PAPI? Multiple Concurrent Operations GLS 3.2 0 vs ILS 3 0 spacing? Service Volume? GBAS VDB vs other NAVAIDs VHF? Offset for Noise? Spacing reduction? How much?

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