DE602007002301D1 - Verfahren zur steuerung eines flugzeuges im landeanflug - Google Patents

Verfahren zur steuerung eines flugzeuges im landeanflug

Info

Publication number
DE602007002301D1
DE602007002301D1 DE602007002301T DE602007002301T DE602007002301D1 DE 602007002301 D1 DE602007002301 D1 DE 602007002301D1 DE 602007002301 T DE602007002301 T DE 602007002301T DE 602007002301 T DE602007002301 T DE 602007002301T DE 602007002301 D1 DE602007002301 D1 DE 602007002301D1
Authority
DE
Germany
Prior art keywords
landeanflug
plane
controlling
high lift
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
DE602007002301T
Other languages
English (en)
Inventor
Franck Delaplace
Martin Richter
Dieter Lang
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 GmbH
Airbus Operations SAS
Original Assignee
Airbus Operations GmbH
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 GmbH, Airbus Operations SAS filed Critical Airbus Operations GmbH
Publication of DE602007002301D1 publication Critical patent/DE602007002301D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/28—Adjustable control surfaces or members, e.g. rudders forming slots by flaps at both the front and rear of the wing operating in unison
    • 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)
  • Toys (AREA)
  • Control Of Turbines (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Electrotherapy Devices (AREA)
  • Measuring Pulse, Heart Rate, Blood Pressure Or Blood Flow (AREA)
  • Tires In General (AREA)
  • Peptides Or Proteins (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Radio Relay Systems (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
DE602007002301T 2006-06-13 2007-06-07 Verfahren zur steuerung eines flugzeuges im landeanflug Active DE602007002301D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0605237A FR2902078B1 (fr) 2006-06-13 2006-06-13 Procede de pilotage d'un aeronef en phase d'approche
PCT/FR2007/000940 WO2007144485A1 (fr) 2006-06-13 2007-06-07 Procede de pilotage d'un aeronef en phase d'approche

Publications (1)

Publication Number Publication Date
DE602007002301D1 true DE602007002301D1 (de) 2009-10-15

Family

ID=37762356

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007002301T Active DE602007002301D1 (de) 2006-06-13 2007-06-07 Verfahren zur steuerung eines flugzeuges im landeanflug

Country Status (11)

Country Link
US (1) US9457888B2 (de)
EP (1) EP2027518B8 (de)
JP (1) JP5112425B2 (de)
CN (1) CN101467114B (de)
AT (1) ATE441886T1 (de)
BR (1) BRPI0711001A2 (de)
CA (1) CA2653638C (de)
DE (1) DE602007002301D1 (de)
FR (1) FR2902078B1 (de)
RU (1) RU2389647C1 (de)
WO (1) WO2007144485A1 (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8451144B2 (en) * 2009-02-04 2013-05-28 Honeywell International Inc. Flaps overspeed advisory system
FR2955309B1 (fr) * 2010-01-18 2013-05-10 Airbus Operations Sas Systeme de commande de vol pour un aeronef
DE102012001268A1 (de) * 2012-01-23 2013-07-25 Airbus Operations Gmbh Verfahren zur Planung eines Landeanflugs eines Flugzeugs, Computerprogrammprodukt, Medium mit einem darauf gespeicherten Landeanflugplan sowie Vorrichtung zur Planung eines Landeanflugs
CA2902927C (en) 2013-03-06 2021-07-06 Bombardier Inc. High lift control method and system for aircraft
EP3307618B1 (de) * 2015-06-12 2019-09-11 Bombardier Inc. Indikatorsysteme, vorrichtungen und verfahren für flugsteuerungsflächen eines flugzeuges mit hohem auftrieb
FR3058016B1 (fr) 2016-10-21 2019-08-23 Airbus Operations Procede et dispositif de gestion de configurations d'un aeronef.
CN113386949A (zh) * 2021-08-16 2021-09-14 中国商用飞机有限责任公司 用于控制飞行器的襟翼和/或缝翼的控制系统和飞行器

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56112398A (en) * 1980-02-09 1981-09-04 Nippon Electric Co Automatic landing raising system for aircraft
JPS63108898U (de) * 1987-01-07 1988-07-13
JP3180115B2 (ja) * 1989-02-27 2001-06-25 良雄 野崎 Ｓｔｏｌ航空機
GB8915487D0 (en) * 1989-07-06 1989-08-23 Short Brothers Plc A flap assembly
FR2817535B1 (fr) 2000-12-06 2003-03-21 Eads Airbus Sa Systeme pour commander automatiquement des dispositifs hypersustentateurs d'un aeronef durant le decollage
FR2857760B1 (fr) * 2003-07-15 2005-09-23 Airbus France Systeme pour commander automatiquement des dispositifs hypersustentateurs d'un aeronef, en particulier des becs de bord d'attaque d'aile.
FR2901537B1 (fr) * 2006-05-29 2008-07-04 Airbus France Sas Procede et dispositif de pilotage d'un aeronef optimisant la commande des ailerons en configuration hypersustentee

Also Published As

Publication number Publication date
JP2009539693A (ja) 2009-11-19
EP2027518B1 (de) 2009-09-02
CN101467114B (zh) 2011-06-08
RU2389647C1 (ru) 2010-05-20
US9457888B2 (en) 2016-10-04
JP5112425B2 (ja) 2013-01-09
CA2653638C (fr) 2015-12-29
FR2902078B1 (fr) 2008-07-11
BRPI0711001A2 (pt) 2011-08-23
FR2902078A1 (fr) 2007-12-14
CA2653638A1 (fr) 2007-12-21
US20090152403A1 (en) 2009-06-18
EP2027518A1 (de) 2009-02-25
CN101467114A (zh) 2009-06-24
WO2007144485A1 (fr) 2007-12-21
ATE441886T1 (de) 2009-09-15
EP2027518B8 (de) 2009-11-11

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Legal Events

Date Code Title Description
8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS OPERATIONS, TOULOUSE, FR

Owner name: AIRBUS DEUTSCHLAND GMBH, 21129 HAMBURG, DE

8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS OPERATIONS, TOULOUSE, FR

Owner name: AIRBUS OPERATIONS GMBH, 21129 HAMBURG, DE