The GBAS Landing System GBAS着陆系统

航空发表于 2010-8-22 00:05:22

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航空发表于 2010-8-22 00:06:14

The GBAS Landing System Steve Duenkel Senior Program Manager Aviation Infrastructure Boeing Commercial Aviation Services October 29, 2009 steven.e.duenkel@boeing.com Export Compliance Statement: The following technical data is under the US Export Administration Regulations ECCN: 9E991.d and is controlled for Anti-BOEING is a trademark of Boeing Management Company. Copyright © 2009 Boeing. All rights reserved. Filename.ppt | 1 +1-425-749-8063 Anti terrorism reasons. Citizens from the following countries can not see this presentation unless a US Export License has been obtained: Cuba, N. Korea, Sudan, Syria and Iran GBAS Landing System (GLS) Topics for Today 􀂃 Boeing history with GLS 􀂃 Equipage 􀂃 Training 􀂃 Operational Implementation Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 2 Boeing History with GLS 􀂃 Boeing – NASA Research Program (1995) 􀂃 1000+ successful approaches with (4) prototype Differential GNSS Systems 􀂃 225 successful autolands 􀂃 Led to development of SARPS compliant prototype ground station 􀂃 Boeing decision to develop and certify GLS for the 737NG 􀂃 Production Certification on 737NG (2005) 􀂃 GLS is production option 􀂃 Available with bulletin and retrofit kit Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 3 service kit. Certified 737 GLS Architecture GPS ANT-L GPS ANT L MMR–1/-2 FCC MMR–1/-2 CLOCK 􀂃 GLS is designed to be “ILS-like”. ILS # MMR-1 ADIRU - VDB/LOC A/B EGPWS MMR 1/ MMR–1/-2 MMR–1/-2 MMR–1/-2 VOR/LOC ANT (TAIL) ANT SW#1 PORT B 1 ILS # GNSS L/R NCP ADIRU-L/R NCP - CAP NCP - F/O VDB/LOC FMC L/R MCU MSU MMR–1/-2 MMR–1/-2 ANT SW#2 2 AUDI O MMR-2 DUAL G/S ANT G/S ANT DFDAU SAI ISFD REU MMR–1/-2 DUAL LOC ANT MMR–1/-2 MMR–1 (NOSE) GPS ANT-R GPS ANT - R L/R ND L/R DEU-1 PFD DEU-2 MMR–1/-2 MMR–1/-2 FMC Flight Management Computer MCU Mode Control Unit SAI Standby Attitude Indicator ISFD Integrated Standby Flight Display DEU Display Electronics Unit PFD Primary Flight Display ND Navigation Display VOR VHF Omnidirectional Ranging Receiver MMR Multimode Receiver ADIRU Air Data Inertial Reference Unit NCP Navigation Control Panel LOC Localizer G/S Glideplope GPS Global Positioning System Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 4 DFDAU Digital Flight Data Acquisition Unit REU Remote Electronics Unit FCC Flight Control Computer EGPWS Enhanced Ground Proximity Warning System The Next Generation 737 Flight Deck with GLS Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 5 Navigation Control Panel (Tuning Panel) 􀂃 Select GLS mode 􀂃 Set GLS channel number 􀂃 Select GLS mode “Active” 􀂃 Verify tuning (on PFD) Copyright © 2009 Boeing. All rights reserved. GLS ■ Page 6 GLS - Approach Selection via FMS 􀂃 Line select a "GLS" approach 􀂃 Missed approach" is auto selected 􀂃 "GLS data" is presented Copyright © 2009 Boeing. All rights reserved. GLS ■ Page 7 GLS – Primary Flight Display ILS GLS Copyright © 2009 Boeing. All rights reserved. GLGSo l■ - VPaargige 8 Flight Crew Training 􀂃Training for flight crews current in B737-600/-700/-800/-900 aircraft is established at Level A.. 􀂃 GLS approach procedures and techniques are identical to those of ILS (with 2 minor exceptions): 􀂃 ILS uses a radio frequency whereas the GLS is a channel on the MMR. 􀂃 The navigation reference on the PFD say “GLS” instead of “ILS”. 􀂃 Crew actions while flying a GLS approach are the same as those for an ILS approach. Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 9 GLS on other Boeing Models 􀂃 For the 787 Dreamliner, GLS is a basic capability (2010). 􀂃 For the 747-8, GLS is a basic capability (provisioned for Category III) (2010). 􀂃 For the 777, Boeing is evaluating the potential incorporation of GLS Category III capability. 􀂃 Implementation on other Boeing models is subject to customer demand. Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 10 Future Category III Capability with GBAS 􀂃Boeing & FAA are pursuing cooperative development for Category II/III capability. 􀂃 Standards are Maturing: 􀂃 RTCA MOPS approved by SC-159 􀂃 Draft ICAO SARPS developed – validation is proceeding 􀂃 Revised Total System Architecture 􀂃 Multi-Mode Receiver (MMR) enhancements 􀂃 GPS antenna improvements 􀂃 GBAS Software development to DO- 278 Level A 􀂃 Improved ground station monitoring 􀂃 Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 11 Near term objective: Pursue operational approval for Special Authorization Category II with “Category I” certified GBAS with operational mitigations GBAS Landing System Operational Trials Boeing Participation Bremen Memphis Newark Guam Sydney Boeing supports our valued customers as they seek to make aviation history with initial Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 12 implementation. The “total system” must be in to begin GLS Operations. Regulatory Facility Air Traffic Airline Airplane p Airport & Capability g y Capability + + Capability + Capability Capability + 􀂃 Framework for implementation: Develop the regulatory basis for GBAS & GLS Approve GBAS Design Install & Commission GBAS Facility Equip Aircraft with GLS Train Flight Crews Approve Operations Train ATC Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 13 Introduce GLS Operations GLS equipped aircraft are coming to China. xie xie ! Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 14 Thank you very much! Ground Base Augmentation System Terminology 􀂃Ground Based Augmentation System (GBAS) refers to the ground elements of the system. 􀂃 GBAS Landing System (GLS) refers to the airplane function based on GBAS (Ground Based Augmentation System) service 􀂃 GLS function intended to be Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 15 ILS look-a-like 737NG GLS Flight Trials Rio de Janeiro Brazil (2005) Janeiro, 􀂃 Included 17 total approaches with 11 auto-lands 􀂃 1 planned low-altitude goaround 􀂃 A Head-Up Display (HUD) AIII landing 􀂃 4 low-altitude approaches to assess coverage over the runways at nearby Santos Dumont. 􀂃 GLS performance SBGL SBRJ during nominal equatorial sunset ionospheric conditions was t bl f ti l Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 16 acceptable for operational use with significant margin. RNP to GLS Transitions FD SPD LNAV VNAV PTH GMWH / 220 RW22 8.4 LOC G/S FMC 2200 1710 􀂃 GLS Final 􀂃 RNP RF leg GLS LAND 3 4000 SPD LOC G/S GMWH / 220o RW22 4.4 140 1200 Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 17 Qantas Airways - RNP to GLS Transitions 􀂃 First RNP to GLS operation in revenue service involving 737NG in May 2009 􀂃 Extremely smooth transition 􀂃 Radar & ADS-B data confirm track conformance 􀂃 Fuel saving of 140 kg (168 litres) per flight over conventional radar vectoring to ILS 􀂃 Emission reduction of 440 kg CO2 􀂃 Noise reductions Copyright © 2009 Boeing. All rights reserved. BOEING PROPRIETARY Filename.ppt | 18 737 Flight Deck Master/Caution Mode Select Unit Copyright © 2009 Boeing. All rights reserved. GLS ■ Page 19

elantian 发表于 2010-8-28 23:07:25

谢谢楼主分享

drjones 发表于 2010-9-1 09:48:13

很好！正对此感兴趣！

ganxing 发表于 2010-9-15 00:42:26

xiexie!!!!!!!!!!!!!

ssaaqq 发表于 2010-9-18 18:19:24

xiexie

xiexie!!!!!!!!!!!!!

xiuhuwang 发表于 2010-10-11 22:18:42

谢谢分享，非常有用

wtf001 发表于 2010-10-26 13:57:46

谢谢分享 xiexie

huihuixy 发表于 2010-11-3 21:58:32

感谢感谢！！！

ss3360 发表于 2010-11-30 20:11:34

我想看一看,谢谢分享

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