DE602005000015D1 - Verfahren um die Landung eines Flugzeuges zu verbessern - Google Patents

Verfahren um die Landung eines Flugzeuges zu verbessern

Info

Publication number
DE602005000015D1
DE602005000015D1 DE602005000015T DE602005000015T DE602005000015D1 DE 602005000015 D1 DE602005000015 D1 DE 602005000015D1 DE 602005000015 T DE602005000015 T DE 602005000015T DE 602005000015 T DE602005000015 T DE 602005000015T DE 602005000015 D1 DE602005000015 D1 DE 602005000015D1
Authority
DE
Germany
Prior art keywords
elevators
stabilizer
landing
aircraft
procedure
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
DE602005000015T
Other languages
English (en)
Other versions
DE602005000015T2 (de
Inventor
Regis Boe
Philippe Seve
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 DE602005000015D1 publication Critical patent/DE602005000015D1/de
Application granted granted Critical
Publication of DE602005000015T2 publication Critical patent/DE602005000015T2/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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Radio Relay Systems (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Vehicle Body Suspensions (AREA)
  • Bridges Or Land Bridges (AREA)
  • Soil Working Implements (AREA)
DE602005000015T 2004-02-06 2005-01-10 Verfahren um die Landung eines Flugzeuges zu verbessern Active DE602005000015T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0401134 2004-02-06
FR0401134A FR2865999B1 (fr) 2004-02-06 2004-02-06 Procede pour ameliorer l'atterrissage d'un aeronef.

Publications (2)

Publication Number Publication Date
DE602005000015D1 true DE602005000015D1 (de) 2006-07-20
DE602005000015T2 DE602005000015T2 (de) 2006-11-23

Family

ID=34673904

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005000015T Active DE602005000015T2 (de) 2004-02-06 2005-01-10 Verfahren um die Landung eines Flugzeuges zu verbessern

Country Status (6)

Country Link
US (1) US7201347B2 (de)
EP (1) EP1562091B1 (de)
AT (1) ATE329301T1 (de)
CA (1) CA2491357C (de)
DE (1) DE602005000015T2 (de)
FR (1) FR2865999B1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2885706B1 (fr) * 2005-05-10 2007-06-15 Airbus France Sas Procede d'aide au decollage d'un aeronef.
FR2893909B1 (fr) * 2005-11-29 2007-12-21 Airbus France Sas Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse.
US8331888B2 (en) * 2006-05-31 2012-12-11 The Boeing Company Remote programmable reference
DE102007012425A1 (de) * 2007-03-15 2008-09-18 Airbus Deutschland Gmbh Verfahren und Einrichtung zur Höhenflossentrimmung bei einem Flugzeug
KR100910552B1 (ko) * 2008-08-20 2009-08-03 윙쉽테크놀러지 주식회사 위그선 날개 구조
US9878776B2 (en) * 2014-05-15 2018-01-30 The Boeing Company System and method for optimizing horizontal tail loads
EP3448749B1 (de) * 2016-04-25 2020-07-01 Bombardier Inc. Luftfahrzeugpitchregelungssystem mit elektronisch übersetztem höhenruder
RU2645522C1 (ru) * 2016-09-05 2018-02-21 Сергей Николаевич Низов Планер летательного аппарата
US10816998B2 (en) * 2017-09-18 2020-10-27 The Boeing Company Airplane takeoff trims utilizing both stabilizers and elevators

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2563757A (en) * 1945-07-23 1951-08-07 Lockheed Aircraft Corp All-movable horizontal tail
US4043523A (en) * 1976-03-11 1977-08-23 Ball Brothers Research Corporation Apparatus for aircraft pitch trim
US4261533A (en) * 1978-06-26 1981-04-14 Dynamic Engineering, Inc. All-axis control of aircraft in ultra deep stall
US4291853A (en) * 1978-12-26 1981-09-29 The Boeing Company Airplane all-moving airfoil with moment reducing apex
US4790494A (en) * 1986-10-14 1988-12-13 Grumman Aerospace Corporation Aircraft empennage with fixed trailing edge horizontal stabilizer
US5707029A (en) * 1996-03-07 1998-01-13 Mcintosh; William J. Aileron/elevators and body flap for roll, pitch, and yaw control
US5823479A (en) * 1996-05-20 1998-10-20 The Boeing Company Landing attitude modifier for airplane
US5779191A (en) * 1996-11-12 1998-07-14 Brislawn; Mark G. Pylon flap for increasing negative pitching moments
US6450456B1 (en) * 1999-12-20 2002-09-17 Safe Flight Instrument Corporation Airborne safe landing power control system and method

Also Published As

Publication number Publication date
EP1562091B1 (de) 2006-06-07
FR2865999B1 (fr) 2006-04-07
FR2865999A1 (fr) 2005-08-12
US20050218262A1 (en) 2005-10-06
ATE329301T1 (de) 2006-06-15
CA2491357A1 (fr) 2005-08-06
EP1562091A1 (de) 2005-08-10
DE602005000015T2 (de) 2006-11-23
CA2491357C (fr) 2012-02-07
US7201347B2 (en) 2007-04-10

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