DE602008004482D1 - Verfahren und einrichtung zur höhenflossentrimmung bei einem flugzeug - Google Patents

Verfahren und einrichtung zur höhenflossentrimmung bei einem flugzeug

Info

Publication number
DE602008004482D1
DE602008004482D1 DE602008004482T DE602008004482T DE602008004482D1 DE 602008004482 D1 DE602008004482 D1 DE 602008004482D1 DE 602008004482 T DE602008004482 T DE 602008004482T DE 602008004482 T DE602008004482 T DE 602008004482T DE 602008004482 D1 DE602008004482 D1 DE 602008004482D1
Authority
DE
Germany
Prior art keywords
adjusting
elevator
moveable tail
command
adjusting drive
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
DE602008004482T
Other languages
English (en)
Inventor
Torsten Holzhausen
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
Original Assignee
Airbus Operations GmbH
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 filed Critical Airbus Operations GmbH
Publication of DE602008004482D1 publication Critical patent/DE602008004482D1/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
    • B64C9/04—Adjustable control surfaces or members, e.g. rudders with compound dependent movements
    • 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
    • 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
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Elevator Control (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Apparatus For Radiation Diagnosis (AREA)
DE602008004482T 2007-03-15 2008-03-17 Verfahren und einrichtung zur höhenflossentrimmung bei einem flugzeug Active DE602008004482D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007012425A DE102007012425A1 (de) 2007-03-15 2007-03-15 Verfahren und Einrichtung zur Höhenflossentrimmung bei einem Flugzeug
PCT/EP2008/002100 WO2008110384A1 (en) 2007-03-15 2008-03-17 Method and device for moveable tail trimming in an aircraft

Publications (1)

Publication Number Publication Date
DE602008004482D1 true DE602008004482D1 (de) 2011-02-24

Family

ID=39683436

Family Applications (2)

Application Number Title Priority Date Filing Date
DE102007012425A Ceased DE102007012425A1 (de) 2007-03-15 2007-03-15 Verfahren und Einrichtung zur Höhenflossentrimmung bei einem Flugzeug
DE602008004482T Active DE602008004482D1 (de) 2007-03-15 2008-03-17 Verfahren und einrichtung zur höhenflossentrimmung bei einem flugzeug

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE102007012425A Ceased DE102007012425A1 (de) 2007-03-15 2007-03-15 Verfahren und Einrichtung zur Höhenflossentrimmung bei einem Flugzeug

Country Status (9)

Country Link
US (1) US8489257B2 (de)
EP (1) EP2137067B1 (de)
CN (1) CN101674981B (de)
AT (1) ATE495096T1 (de)
BR (1) BRPI0808743A2 (de)
CA (1) CA2680637A1 (de)
DE (2) DE102007012425A1 (de)
RU (1) RU2460670C2 (de)
WO (1) WO2008110384A1 (de)

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* Cited by examiner, † Cited by third party
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DE102007012425A1 (de) * 2007-03-15 2008-09-18 Airbus Deutschland Gmbh Verfahren und Einrichtung zur Höhenflossentrimmung bei einem Flugzeug
US9085371B2 (en) 2008-11-20 2015-07-21 The Boeing Company Automatic throttle roll angle compensation
US9058040B2 (en) * 2009-02-27 2015-06-16 The Boeing Company Automatic pilot pitch angle compensation
US8718839B2 (en) * 2009-12-06 2014-05-06 Evolved Aircraft Systems, L.L.C. Method and apparatus for automatically controlling aircraft flight control trim systems
CN102229357B (zh) * 2011-05-12 2013-07-03 北京航空航天大学 具有安装角可调节平尾的尾翼
FR2980453B1 (fr) * 2011-09-26 2014-06-27 Airbus Operations Sas Systeme electrique de commande de direction pour aeronef
FR2986065B1 (fr) * 2012-01-23 2015-04-17 Airbus Operations Sas Procede et dispositif d'affichage d'informations d'assiette sur un avion lors d'un decollage.
FR3002334B1 (fr) * 2013-02-19 2016-07-15 Airbus Operations Sas Procede et dispositif d'estimation d'un moment de tangage non desire d'un avion, et applications au controle du tangage de l'avion.
US9878776B2 (en) * 2014-05-15 2018-01-30 The Boeing Company System and method for optimizing horizontal tail loads
CN104401503B (zh) * 2014-10-23 2016-06-01 中国运载火箭技术研究院 一种适用于多舵面再入飞行器的配平舵偏角确定方法
US9731813B2 (en) * 2014-11-12 2017-08-15 The Boeing Company Methods and apparatus to control aircraft horizontal stabilizers
EP3448749B1 (de) 2016-04-25 2020-07-01 Bombardier Inc. Luftfahrzeugpitchregelungssystem mit elektronisch übersetztem höhenruder
US10259564B2 (en) * 2016-08-08 2019-04-16 Gulfstream Aerospace Corporation Controlling elevator to stabilizer offload in fly-by-wire aircraft systems
DE102016117634B4 (de) * 2016-09-19 2019-12-12 Deutsches Zentrum für Luft- und Raumfahrt e.V. Steuerung und Regelung von Aktoren, die aerodynamische Steuerflächen eines Luftfahrzeugs antreiben
FR3057370B1 (fr) * 2016-10-11 2019-08-23 Airbus Operations Procede et systeme de commande de vol d'un aeronef.
US10816998B2 (en) * 2017-09-18 2020-10-27 The Boeing Company Airplane takeoff trims utilizing both stabilizers and elevators
CN109703780B (zh) * 2018-10-26 2022-04-19 中国飞行试验研究院 一种电传运输类飞机飞行试验舵面卡阻实现方法
CN112623192B (zh) * 2020-12-29 2022-10-11 中国航空工业集团公司西安飞机设计研究所 一种飞机方向舵自动配平控制方法
CN113479316B (zh) * 2021-09-08 2021-11-30 中国商用飞机有限责任公司 用于控制飞行器的平尾卸载的方法、系统和介质

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US3682417A (en) * 1970-04-06 1972-08-08 Lear Siegler Inc Engagement of altitude hold mode in aircraft flight control system
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US3719878A (en) * 1971-09-27 1973-03-06 Sperry Rand Corp Digital automatic control system with pseudo position feedback and monitor
US3848833A (en) * 1972-07-14 1974-11-19 Sperry Rand Corp Aircraft automatic flight control system
US4129275A (en) * 1974-11-22 1978-12-12 The Boeing Company Automatic flight control apparatus for aircraft
US4032093A (en) * 1975-06-27 1977-06-28 The Boeing Company Adaptive energy management for vertical speed control of an aircraft
US4021009A (en) * 1975-07-24 1977-05-03 Sperry Rand Corporation Vertical path control for aircraft area navigation system
US4304375A (en) * 1979-05-17 1981-12-08 Textron Inc. Electrically controlled elevator
SU788594A1 (ru) * 1979-09-28 2005-04-20 Л.Р. Львов Устройство управления стабилизатором самолета
US4347572A (en) * 1979-11-02 1982-08-31 The Boeing Company Method and apparatus for an aircraft climb-out guidance system
US4382282A (en) * 1980-09-08 1983-05-03 Sperry Corporation Trim control system for reduced drag
SU1029539A1 (ru) * 1981-10-21 1995-07-09 М.Л. Пхор Система автоматического управления стабилизатором самолета
SU1129837A1 (ru) * 1983-01-25 2004-12-27 Ю.Б. Константинов Система автоматической продольной балансировки самолета
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FR2661149B1 (fr) * 1990-04-24 1992-08-14 Aerospatiale Systeme pour le pilotage d'un avion en tangage.
FR2664231B1 (fr) * 1990-07-04 1992-10-09 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.
US5692708A (en) * 1995-05-15 1997-12-02 The Boeing Company Method and apparatus for automatically trimming an airplane stabilizer
FR2771998B1 (fr) * 1997-12-08 2000-02-25 Sfim Ind Actionneur de gouverne de commande de vol d'aeronef
US6591169B2 (en) * 2001-09-27 2003-07-08 The Boeing Company Method and computer program product for controlling the actuators of an aerodynamic vehicle
FR2864023B1 (fr) * 2003-12-19 2006-03-03 Airbus France Procede pour ameliorer la manoeuvrabilite d'un aeronef lors d'une ressource.
FR2865999B1 (fr) * 2004-02-06 2006-04-07 Airbus France Procede pour ameliorer l'atterrissage d'un aeronef.
FR2869588B1 (fr) * 2004-04-28 2006-07-14 Airbus France Sas Procede d'aide au decollage d'un aeronef.
DE102004047008A1 (de) * 2004-09-28 2006-03-30 Liebherr-Aerospace Lindenberg Gmbh Vorrichtung zur Einstellung von Flugzeughöhenflossen
DE102007012425A1 (de) * 2007-03-15 2008-09-18 Airbus Deutschland Gmbh Verfahren und Einrichtung zur Höhenflossentrimmung bei einem Flugzeug
US9058040B2 (en) * 2009-02-27 2015-06-16 The Boeing Company Automatic pilot pitch angle compensation

Also Published As

Publication number Publication date
BRPI0808743A2 (pt) 2014-08-19
CN101674981A (zh) 2010-03-17
US20100042271A1 (en) 2010-02-18
WO2008110384A1 (en) 2008-09-18
EP2137067A1 (de) 2009-12-30
WO2008110384B1 (en) 2008-12-11
RU2460670C2 (ru) 2012-09-10
DE102007012425A1 (de) 2008-09-18
ATE495096T1 (de) 2011-01-15
RU2009137785A (ru) 2011-04-20
CN101674981B (zh) 2012-06-27
EP2137067B1 (de) 2011-01-12
US8489257B2 (en) 2013-07-16
CA2680637A1 (en) 2008-09-18

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