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DE602007001136D1 - Vorrichtung zur unterstützung der flugzeuglenkung in der landeanflugsphase zum landen - Google Patents

Vorrichtung zur unterstützung der flugzeuglenkung in der landeanflugsphase zum landen

Info

Publication number
DE602007001136D1
DE602007001136D1 DE602007001136T DE602007001136T DE602007001136D1 DE 602007001136 D1 DE602007001136 D1 DE 602007001136D1 DE 602007001136 T DE602007001136 T DE 602007001136T DE 602007001136 T DE602007001136 T DE 602007001136T DE 602007001136 D1 DE602007001136 D1 DE 602007001136D1
Authority
DE
Germany
Prior art keywords
country
land
landing phase
aircraft management
supporting aircraft
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
DE602007001136T
Other languages
English (en)
Inventor
Patrice Rouquette
Jean-Philippe Huynh
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of DE602007001136D1 publication Critical patent/DE602007001136D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/50—Navigation or guidance aids
    • G08G5/54—Navigation or guidance aids for approach or landing
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/20—Arrangements for acquiring, generating, sharing or displaying traffic information
    • G08G5/21—Arrangements for acquiring, generating, sharing or displaying traffic information located onboard the aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Networks Using Active Elements (AREA)
DE602007001136T 2006-02-20 2007-02-14 Vorrichtung zur unterstützung der flugzeuglenkung in der landeanflugsphase zum landen Active DE602007001136D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0601453A FR2897712B1 (fr) 2006-02-20 2006-02-20 Dispositif d'aide au pilotage d'un aeronef lors d'une phase d'approche en vue d'un atterrissage.
PCT/FR2007/000258 WO2007096500A1 (fr) 2006-02-20 2007-02-14 Dispositif d’aide au pilotage d’un aeronef lors d’une phase d’approche en vue d’un atterrissage

Publications (1)

Publication Number Publication Date
DE602007001136D1 true DE602007001136D1 (de) 2009-06-25

Family

ID=37054359

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007001136T Active DE602007001136D1 (de) 2006-02-20 2007-02-14 Vorrichtung zur unterstützung der flugzeuglenkung in der landeanflugsphase zum landen

Country Status (11)

Country Link
US (1) US8112188B2 (de)
EP (1) EP1987503B1 (de)
JP (1) JP5112339B2 (de)
CN (1) CN101385058B (de)
AT (1) ATE431606T1 (de)
BR (1) BRPI0706972A2 (de)
CA (1) CA2640318C (de)
DE (1) DE602007001136D1 (de)
FR (1) FR2897712B1 (de)
RU (1) RU2381563C1 (de)
WO (1) WO2007096500A1 (de)

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FR3010807B1 (fr) * 2013-09-13 2015-10-09 Airbus Operations Sas Procede et dispositif d'aide au pilotage d'un aeronef lors d'une phase d'approche en vue d'un atterrissage.
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FR3016223B1 (fr) * 2014-01-03 2017-03-10 Airbus Operations Sas Procede et dispositif de determination d'un profil de terrain lineaire le long d'une trajectoire laterale d'approche d'un aeroport.
FR3016222B1 (fr) 2014-01-03 2016-02-05 Airbus Operations Sas Procede et dispositif de guidage vertical d'un aeronef lors d'une approche d'une piste d'atterrissage le long d'une trajectoire laterale d'approche.
FR3017703B1 (fr) * 2014-02-14 2017-12-22 Thales Sa Procede et systeme de determination de la compatibilite d'un guidage angulaire avec une approche
US9704405B2 (en) * 2014-06-12 2017-07-11 Honeywell International Inc. Aircraft display systems and methods for providing an aircraft display for use with airport departure and arrival procedures
FR3024229B1 (fr) * 2014-07-23 2016-12-09 Airbus Operations Sas Procede et dispositif de gestion automatique d'operations aeriennes necessitant une garantie de performance de navigation et de guidage d'un aeronef.
GB2529682A (en) * 2014-08-29 2016-03-02 Bae Systems Plc Image display
WO2016059930A1 (ja) 2014-10-17 2016-04-21 ソニー株式会社 装置、方法及びプログラム
US10540904B2 (en) * 2015-05-08 2020-01-21 Bombardier Inc. Systems and methods for assisting with aircraft landing
FR3039691B1 (fr) * 2015-07-31 2017-07-21 Airbus Operations Sas Procede et systeme d'aide au guidage d'un aeronef le long d'un axe d'approche d'une piste d'atterrissage
US9989972B2 (en) * 2016-02-22 2018-06-05 The Boeing Company Systems and methods to prevent an aircraft from tail contact with the ground
US9672749B1 (en) * 2016-04-08 2017-06-06 Honeywell International Inc. System and method for updating ILS category and decision height
FR3058016B1 (fr) * 2016-10-21 2019-08-23 Airbus Operations Procede et dispositif de gestion de configurations d'un aeronef.
US20190236965A1 (en) * 2018-01-29 2019-08-01 Honeywell International Inc. System and method for providing prioritized alternate approach procedures
CN108646785B (zh) * 2018-06-22 2020-12-29 西安飞机工业（集团）有限责任公司 一种飞机的飞行指引系统及改进方法
DE102018120198A1 (de) * 2018-08-20 2020-02-20 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
RU2708785C1 (ru) * 2018-12-11 2019-12-11 Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации Способ автоматического управления продольным движением летательного аппарата на посадке
FR3098628B1 (fr) * 2019-07-08 2021-09-10 Thales Sa Procede et systeme electronique de gestion du vol d'un aeronef en phase d'approche visuelle vers une piste d'atterrissage, programme d'ordinateur associe
US11682307B2 (en) 2020-07-07 2023-06-20 Honeywell International Inc. Situation-aware, intelligent data-synchronization methods for UAV-inspection applications
US11676499B2 (en) * 2021-06-17 2023-06-13 Honeywell International Inc. Methods and systems for alerting a visual descent point (VDP)
CN114722133B (zh) * 2022-03-30 2024-11-12 中国人民解放军空军工程大学 一种微波着陆系统航图标注方法、存储介质及系统
US20240177616A1 (en) * 2022-11-29 2024-05-30 Rockwell Collins, Inc. System and method for enhancing pilot situational awareness for hybrid approach procedure sets

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Also Published As

Publication number Publication date
RU2381563C1 (ru) 2010-02-10
EP1987503A1 (de) 2008-11-05
US8112188B2 (en) 2012-02-07
CN101385058A (zh) 2009-03-11
CN101385058B (zh) 2011-07-06
FR2897712B1 (fr) 2008-04-04
JP2009527399A (ja) 2009-07-30
WO2007096500A1 (fr) 2007-08-30
ATE431606T1 (de) 2009-05-15
JP5112339B2 (ja) 2013-01-09
BRPI0706972A2 (pt) 2011-04-12
CA2640318A1 (fr) 2007-08-30
FR2897712A1 (fr) 2007-08-24
CA2640318C (fr) 2015-04-21
EP1987503B1 (de) 2009-05-13
US20090024261A1 (en) 2009-01-22

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