ATE400498T1 - Verfahren und system zum verschieben eines flugzeugseitenruders - Google Patents

Verfahren und system zum verschieben eines flugzeugseitenruders

Info

Publication number
ATE400498T1
ATE400498T1 AT03291892T AT03291892T ATE400498T1 AT E400498 T1 ATE400498 T1 AT E400498T1 AT 03291892 T AT03291892 T AT 03291892T AT 03291892 T AT03291892 T AT 03291892T AT E400498 T1 ATE400498 T1 AT E400498T1
Authority
AT
Austria
Prior art keywords
force
rudder
moving
aircraft rudder
order
Prior art date
Application number
AT03291892T
Other languages
English (en)
Inventor
De Kreeke Marc Van
Guillaume Cassein
Original Assignee
Airbus France
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 France filed Critical Airbus France
Application granted granted Critical
Publication of ATE400498T1 publication Critical patent/ATE400498T1/de

Links

Classifications

    • 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
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Control Devices (AREA)
  • Regulating Braking Force (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
  • Radio Relay Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
AT03291892T 2002-09-09 2003-07-30 Verfahren und system zum verschieben eines flugzeugseitenruders ATE400498T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0211124A FR2844251B1 (fr) 2002-09-09 2002-09-09 Procede et systeme pour deplacer une gouverne d'un aeronef.

Publications (1)

Publication Number Publication Date
ATE400498T1 true ATE400498T1 (de) 2008-07-15

Family

ID=31503138

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03291892T ATE400498T1 (de) 2002-09-09 2003-07-30 Verfahren und system zum verschieben eines flugzeugseitenruders

Country Status (6)

Country Link
US (1) US6928340B2 (de)
EP (1) EP1396421B1 (de)
AT (1) ATE400498T1 (de)
CA (1) CA2437216C (de)
DE (1) DE60322002D1 (de)
FR (1) FR2844251B1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7593793B2 (en) * 2004-07-30 2009-09-22 The Boeing Company Adaptive control in the presence of input constraints
FR2891051B1 (fr) * 2005-09-22 2007-10-19 Airbus France Sas Procede et dispositif pour realiser au moins un essai en vol sur un aeronef et applications
FR2892699B1 (fr) * 2005-10-27 2008-02-08 Airbus France Sas Procede et systeme de limitation d'un angle de braquage de la gouverne d'un aeronef
FR2897838B1 (fr) * 2006-02-27 2009-01-09 Airbus France Sas Systeme de commande electrique pour une gouverne de direction d'un avion.
US8245967B2 (en) 2008-11-25 2012-08-21 The Boeing Company Actuator force equalization controller
US8504221B2 (en) * 2009-01-16 2013-08-06 The Boeing Company Apparatus and method for controlling a control surface of a vehicle based on a load identified on the control surface
FR2959575B1 (fr) * 2010-05-03 2014-08-29 Airbus Operations Sas Procede et dispositif pour la reduction des charges engendrees sur un avion par une perturbation aerodynamique.
US9821903B2 (en) * 2014-07-14 2017-11-21 The Boeing Company Closed loop control of aircraft control surfaces
CN109521750B (zh) * 2018-03-16 2021-12-03 陕西飞机工业（集团）有限公司 一种停机制动操纵系统

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5170969A (en) * 1988-11-23 1992-12-15 The Boeing Company Aircraft rudder command system
EP0488428A3 (en) * 1990-09-24 1992-10-14 The Boeing Company Apparatus and method for reducing aircraft loads resulting from atmospheric turbulence and gusts
US6539290B1 (en) * 1995-06-07 2003-03-25 Dabulamanzi Holdings, Llc Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation
US6209825B1 (en) * 1998-02-27 2001-04-03 Lockheed Martin Corporation Low power loss electro hydraulic actuator
FR2793765B1 (fr) * 1999-05-18 2001-07-13 Eurocopter France Dispositif de commande de vol d'un aeronef
FR2809373B1 (fr) 2000-05-29 2002-08-09 Aerospatiale Matra Airbus Systeme de commande electrique pour une gouverne de direction d'aeronef

Also Published As

Publication number Publication date
DE60322002D1 (de) 2008-08-21
US20040111190A1 (en) 2004-06-10
CA2437216A1 (fr) 2004-03-09
FR2844251A1 (fr) 2004-03-12
EP1396421A1 (de) 2004-03-10
FR2844251B1 (fr) 2005-05-27
EP1396421B1 (de) 2008-07-09
CA2437216C (fr) 2011-02-15
US6928340B2 (en) 2005-08-09

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Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties