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DE602007011757D1 - Landehilfevorrichtung und verfahren für ein flugzeug - Google Patents

Landehilfevorrichtung und verfahren für ein flugzeug

Info

Publication number
DE602007011757D1
DE602007011757D1 DE602007011757T DE602007011757T DE602007011757D1 DE 602007011757 D1 DE602007011757 D1 DE 602007011757D1 DE 602007011757 T DE602007011757 T DE 602007011757T DE 602007011757 T DE602007011757 T DE 602007011757T DE 602007011757 D1 DE602007011757 D1 DE 602007011757D1
Authority
DE
Germany
Prior art keywords
plane
agricultural apparatus
total energy
aircraft
landing
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
DE602007011757T
Other languages
English (en)
Inventor
Florian Constans
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 DE602007011757D1 publication Critical patent/DE602007011757D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)
  • Radio Relay Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Catching Or Destruction (AREA)
DE602007011757T 2006-06-12 2007-06-07 Landehilfevorrichtung und verfahren für ein flugzeug Active DE602007011757D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0605157A FR2902081B1 (fr) 2006-06-12 2006-06-12 Procede et dispositif d'assistance a l'atterissage pour aeronef
PCT/FR2007/000939 WO2007144484A1 (fr) 2006-06-12 2007-06-07 Procede et dispositif d'assistance a l'atterrissage pour aeronef

Publications (1)

Publication Number Publication Date
DE602007011757D1 true DE602007011757D1 (de) 2011-02-17

Family

ID=37801470

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007011757T Active DE602007011757D1 (de) 2006-06-12 2007-06-07 Landehilfevorrichtung und verfahren für ein flugzeug

Country Status (11)

Country Link
US (1) US7952492B2 (de)
EP (1) EP2035281B1 (de)
JP (1) JP5209615B2 (de)
CN (1) CN101466599B (de)
AT (1) ATE494215T1 (de)
BR (1) BRPI0711662A2 (de)
CA (1) CA2652654C (de)
DE (1) DE602007011757D1 (de)
FR (1) FR2902081B1 (de)
RU (1) RU2389659C1 (de)
WO (1) WO2007144484A1 (de)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
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FR2946173B1 (fr) * 2009-05-27 2011-07-15 Airbus France Procede et dispositif d'engagement d'un mode de pilotage automatique d'un aeronef.
US8494693B2 (en) * 2009-08-05 2013-07-23 The Boeing Company Vertical required navigation performance containment with radio altitude
FR2956512B1 (fr) 2010-02-16 2012-03-09 Airbus Operations Sas Procede et dispositif de protection automatique d'un aeronef contre un taux de descente excessif.
CN101944295B (zh) * 2010-09-08 2012-01-11 北京航空航天大学 一种无人机起落航线编排方法
US8532848B2 (en) * 2010-10-19 2013-09-10 Honeywell International Inc. Systems and methods for alerting potential tailstrike during landing
FR2975796B1 (fr) 2011-05-26 2015-05-01 Airbus Operations Sas Procede et systeme d'aide au pilotage d'un avion lors d'une approche
FR2978282B1 (fr) * 2011-07-22 2013-08-30 Thales Sa Procede et dispositif pour le filtrage d'alertes provenant d'un systeme de detection de collision d'un aeronef
FR2978588B1 (fr) * 2011-07-29 2016-03-11 Airbus Operations Sas Procede et dispositif de gestion optimisee de l'utilisation des becs et des volets, ainsi que du train d'atterrissage d'un aeronef
FR2978736B1 (fr) * 2011-08-01 2013-09-27 Airbus Operations Sas Dispositif et procede de determination d'un etat de piste, aeronef comprenant un tel dispositif et systeme d'aide au pilotage exploitant cet etat de piste
CN102390543B (zh) * 2011-08-23 2013-07-24 北京航空航天大学 一种无人机的纵向着陆轨迹的设计方法
FR2986876B1 (fr) * 2012-02-15 2014-12-05 Airbus Detection d'anomalie de descente d'un aeronef
IL218327A (en) * 2012-02-26 2013-05-30 Elbit Systems Ltd Safe emergency landing of unmanned aerial vehicles
RU2509037C1 (ru) * 2012-07-19 2014-03-10 Федеральное государственное бюджетное учреждение науки Институт проблем управления им. В.А. Трапезникова Российской академии наук Способ формирования командного индекса для управления тягой двигателя самолета и устройство для его реализации
US8918234B2 (en) 2012-09-17 2014-12-23 Bell Helicopter Textron Inc. Landing point indication system
US9221554B2 (en) * 2013-03-06 2015-12-29 Gulfstream Aerospace Corporation Runway overrun monitor
FR3005760B1 (fr) * 2013-05-17 2017-10-20 Airbus Operations Sas Procede et dispositif de determination automatique d'un profil optimise d'approche et/ou de descente pour un aeronef.
US9026275B1 (en) * 2013-07-24 2015-05-05 Shih-Yih Young In-flight generation of RTA-compliant optimal profile descent paths
US20150348423A1 (en) * 2014-05-27 2015-12-03 Honeywell International Inc. System and method for economizing flight expenditures during aircraft descent and approach
DE102014014446A1 (de) * 2014-09-26 2016-03-31 Airbus Defence and Space GmbH Redundantes Bestimmen von Positionsdaten für ein automatisches Landesystem
US9499279B2 (en) * 2014-09-26 2016-11-22 Honeywell International Inc. System and method for displaying runway approach information
US9399524B2 (en) * 2014-10-21 2016-07-26 Honeywell International Inc. System and method for displaying runway landing information
US9815571B1 (en) * 2015-03-04 2017-11-14 Rockwell Collins, Inc. Aircraft energy indicator generating system, device, and method
FR3043473B1 (fr) * 2015-11-05 2017-11-24 Airbus Operations Sas Procede et dispositif d'aide au pilotage d'un aeronef pour une gestion de l’energie lors d’une phase d’approche.
US10325507B2 (en) 2016-10-06 2019-06-18 Honeywell International Inc. Method and system for determining effective approach angle and predicting aircraft landing distance
CN106586004A (zh) * 2016-12-05 2017-04-26 中国航空工业集团公司洛阳电光设备研究所 一种飞机着陆擦尾告警方法
CN108241377B (zh) * 2017-12-08 2020-12-29 中国航空工业集团公司成都飞机设计研究所 一种基于航程航时性能的无人机自动高度缓降控制方法
US10569898B2 (en) * 2018-03-26 2020-02-25 Honeywell International Inc. Method and system for generating an alert for an aircraft potentially exceeding speed limits in restricted airspace
JP7036220B2 (ja) * 2018-08-22 2022-03-15 日本電気株式会社 選定装置、選定方法及び選定プログラム
CN109144079B (zh) * 2018-08-22 2021-04-23 中国民航大学 一种基于综合化航电的水陆两栖飞机降落构型控制系统
CN109506662B (zh) * 2018-10-30 2020-09-18 北京控制工程研究所 一种小天体着陆初始对准方法、其相对导航基准确定方法及装置

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR601395A (fr) 1925-07-29 1926-03-01 Self protégée pour t. s. f.
US4021009A (en) * 1975-07-24 1977-05-03 Sperry Rand Corporation Vertical path control for aircraft area navigation system
US4133503A (en) * 1975-08-29 1979-01-09 Bliss John H Entry, display and use of data employed to overcome aircraft control problems due to wind shear
US4021010A (en) * 1975-08-29 1977-05-03 Bliss John H Method and apparatus to overcome aircraft control problems due to wind shear
US4801110A (en) * 1987-12-21 1989-01-31 Honeywell Inc. Approach to hover control system for helicopters
US5020747A (en) * 1990-01-26 1991-06-04 The Boeing Company Method and apparatus for controlling flare engagement height in automatic landing systems
JPH03120297U (de) * 1990-03-22 1991-12-10
US5206654A (en) * 1992-05-19 1993-04-27 Hughes Aircraft Company Passive aircraft monitoring system
US5823479A (en) * 1996-05-20 1998-10-20 The Boeing Company Landing attitude modifier for airplane
JP2002092799A (ja) * 2000-09-19 2002-03-29 Toshiba Corp 着陸誘導診断システム
US6711478B2 (en) * 2000-12-15 2004-03-23 Garmin At, Inc. Receiver-autonomous vertical integrity monitoring
US6711479B1 (en) * 2001-08-30 2004-03-23 Honeywell International, Inc. Avionics system for determining terminal flightpath
US7132960B2 (en) * 2002-10-15 2006-11-07 Honeywell International Inc. Approach monitoring and advisory system and method
US20040167685A1 (en) * 2003-02-24 2004-08-26 Ryan Dean E. Runway overrun monitor and method for monitoring runway overruns
US7611098B2 (en) * 2005-01-19 2009-11-03 Airbus France Flight management process for an aircraft

Also Published As

Publication number Publication date
EP2035281A1 (de) 2009-03-18
FR2902081B1 (fr) 2008-07-11
CA2652654C (fr) 2014-01-28
CN101466599B (zh) 2011-05-25
EP2035281B1 (de) 2011-01-05
US7952492B2 (en) 2011-05-31
ATE494215T1 (de) 2011-01-15
JP5209615B2 (ja) 2013-06-12
RU2389659C1 (ru) 2010-05-20
CN101466599A (zh) 2009-06-24
BRPI0711662A2 (pt) 2011-11-16
CA2652654A1 (fr) 2007-12-21
US20090195413A1 (en) 2009-08-06
FR2902081A1 (fr) 2007-12-14
JP2009539692A (ja) 2009-11-19
WO2007144484A1 (fr) 2007-12-21

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