avionics support for gbas and performance based … reines icao … · avionics support for gbas...
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![Page 2: Avionics Support for GBAS and Performance Based … Reines ICAO … · Avionics Support for GBAS and Performance Based Navigation (PBN) Pat Reines (pat.reines@honeywell.com))](https://reader034.vdocuments.us/reader034/viewer/2022052309/5ab6e9a97f8b9a0f058e63fa/html5/thumbnails/2.jpg)
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26 ILS Approaches = 26 Localizers and Glide Slopes
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26 ILS Approaches = 26 Localizers and Glide Slope
= 1 GBAS
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26 ILS Approaches = 26 Localizers and Glide Slope
= 1 GBAS
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© 2015 Honeywell International
DRAFT – Protected by the Attorney-Client Privilege/Produced at the Request of Counsel Preliminary – not final – no decision will be taken without satisfaction of any applicable consultation or negotiation requirements
Increases Capacity; Reduces Delays
GBAS Benefits for Next Gen ATM
3.2 degree Glide-slope
2.5 degree Glide-slope
RNP Approach:• curved final approach• begins on the downwind leg• lateral and vertical guidance
• to the runway • or to a GLS intercept
CO2 emission reductions of 1.4243lkg per each 1kg of fuel saved
4 NM final can save up to 10.6 NM/Approach
• 3 minutes of flight time• 82.7 kilograms of fuel• 104 liters of fuel
Reduce Fuel Consumption; Minimize Emissions; Avoid Terrain Reduce Maintenance Costs; Increase Precision Approaches
Flexible Approach Geometries Requires No “Clear Zones”
Serves All Runway EndsEnables Efficient Flight Path
Increased Capacity; Reduced Noise; Reduced Track Miles; Reduced Operating Costs
Increase Capacity, Reduces Noise
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VHF Broadcast• Corrections, Integrity,
Approaches• Horizontally Polarized,
Omni-Directional• 108-118 MHz• 2 TDMA Time Slots • 2 Hz Corrections• Redundant Radio
Dual Processor Channels• Differential Corrections• Overall System Integrity• Approach Database• Redundant Channel
Maintenance Data Terminal• System Status, Mode, Control• System Alerts, Alarms• Approach Control
Air Traffic Status Unit• System Mode• System Availability
Reference Receivers• Multipath Limiting Antenna (MLA)• Narrow Correlator GPS Receiver• 2 Hz Measurements• 4 GPS Receivers
1300mMAX
100mMAX
Airport LAN
TDMA – Time Division Multiple AccessHz – HertzLAN – Local Area Network (typ. Ethernet)
Honeywell SmartPath® GBAS
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Multi-Mode Receiver Functionality
GPS
Antenna
DGPS Computes Differential
CorrectionsProvides Integrity
Check Provides Approach
Coordinates
Differential Corrections,Integrity Status and
Approach Coordinates
TransmitterEncoder Decoder
Receiver
Data BroadcastMonitor
Broadcast Information
DATALINK – VHF Data Broadcast (VDB)
Local Ground Facility
PilotInterface
MMRGPS Antenna
Autopilot
CockpitDisplays
Aircraft
AircraftSurfaces
DGPS – Differential GPSMMR – Multi-Mode Receiver (GPS, VDB, ILS, etc)VDB – VHF Data Broadcast (Link to aircraft)
GPS error corrections, integrity, AND path points
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GLS Uses Existing Aircraft Architecture
GLS – GNSS Landing SystemILS – Instrument Landing System
• ILS look alike– Glideslope– Localizer
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April 201617th IGWG - Airbus status - EYIC - Ref. X34PR1606289 - Issue 1
GLS option on Airbus fleet
GLS option status
A320 familyGLS CAT I with Autoland certified Selected by 18 customers
A330GLS CAT I with Autoland certified Selected by 6 customers
A350GLS CAT I with Autoland certified Selected by 10 customersA380GLS CAT I with Autoland certified Selected by 9 customers GLS CAT I certified on all linefit Airbus
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
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April 201617th IGWG - Airbus status - EYIC - Ref. X34PR1606289 - Issue 1
GLS option on Airbus fleet
Airbus customers
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
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Cost effective retrofit options for out of production airplanes are being explored
Copyright © 2016 Boeing. All rights reserved.
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Over 1500airplanes today
>60airlines with GLS
activated
Copyright © 2016 Boeing. All rights reserved.
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47%Boeing deliveries with
GLS activated
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2%
28%25%
5%
Copyright © 2016 Boeing. All rights reserved.
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30%2%8%
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© 2015 Honeywell International
DRAFT – Protected by the Attorney-Client Privilege/Produced at the Request of Counsel Preliminary – not final – no decision will be taken without satisfaction of any applicable consultation or negotiation requirements
IMMR Approach
2x 3MCU LRUs (22Lbs)
4x 3MCU LRUs (36Lbs)
MMR
GNSS
MMR
GNSS
LOC GS
VOR
VOR
VOR
MB
LOC GS
GNSSiMMR iMMR
VOR
MB
GNSSGNSS ILS & GBAS CAT I/II/III SBAS/EGNOS
Multi-Constellation GNSS LPV / FLS
RNP / RNP-AR
New Navigation Receiver for Future Needs
Today
VOR VOR
MMR MMR
Integrated Multi-Mode Receiver (IMMR)
38%↓
in3
50%↓
14Lbs 650in3
50%Shelf space↓
6 MCU↓
SWaP
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SmartPath Certification Baseline, Growth• SmartPath Cat I System Design and Operational Approvals
– FAA (US): September 2009– BAF (Germany): November 2011– Other approvals: Spain, Australia, Switzerland– In revenue passenger service now
• Block II software/SBAS – SBAS network provides iono status: benign iono enables GBAS
parameter changes– Approved by FAA September 2015– Cat II on Cat I ground station
• No new avionics required– Autoland capability– 48 approaches/ground station– Ionospheric mitigations
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SmartPath Certification Baseline, Growth• Cat III development and validation underway
– Cat I station is upgradeable to Cat III
– Cat III GBAS works with Cat I and Cat II/III GLS avionics
– FAA Cat III ground station/avionics contracts to Honeywell: 2010
• Prototype ground station/avionics based on SLS-4000 and INR
– Flight testing and additional development: 2012-2016
• FAA testing 2012
• SESAR flight tests 2013-2016
• Boeing ecoDemonstrator Cat III autolands 2014
– Certification: 2018
• FAA/Honeywell approval project underway
– Forecasted to be operationally available: 2019
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SmartPath Certification Baseline, Growth
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AirlinesLowers operational cost, and increases schedule reliability
ANSPEnhances safety, environmental impacts, ATM modernization
AirportsImproves capacity, lowers cost, future
proof to CAT III
Stakeholder Involvement Throughout the Whole Project =
Successful Implementation
Value is shared across all stakeholders
Regulator
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x Thank You!