DE60302861D1 - System, das eine Anzeigung von Steuerungsschwingungskupplungen verwendet, zur elektrischen Flugsteuerung eines Flugzeugs, sowie Steuerelement für ein solches System - Google Patents

System, das eine Anzeigung von Steuerungsschwingungskupplungen verwendet, zur elektrischen Flugsteuerung eines Flugzeugs, sowie Steuerelement für ein solches System

Info

Publication number
DE60302861D1
DE60302861D1 DE60302861T DE60302861T DE60302861D1 DE 60302861 D1 DE60302861 D1 DE 60302861D1 DE 60302861 T DE60302861 T DE 60302861T DE 60302861 T DE60302861 T DE 60302861T DE 60302861 D1 DE60302861 D1 DE 60302861D1
Authority
DE
Germany
Prior art keywords
control
pilot
clutches
aircraft
indication
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.)
Expired - Lifetime
Application number
DE60302861T
Other languages
English (en)
Other versions
DE60302861T2 (de
Inventor
Nathalie Raimbault
Jean-Pierre Gautier
Alain Sagansan
Pierre Fabre
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 DE60302861D1 publication Critical patent/DE60302861D1/de
Application granted granted Critical
Publication of DE60302861T2 publication Critical patent/DE60302861T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Vibration Prevention Devices (AREA)
  • Vehicle Body Suspensions (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
  • Toys (AREA)
  • Mechanical Control Devices (AREA)
  • Details Of Aerials (AREA)
  • Position Input By Displaying (AREA)
DE60302861T 2002-11-18 2003-10-23 System, das eine Anzeigung von Steuerungsschwingungskupplungen verwendet, zur elektrischen Flugsteuerung eines Flugzeugs, sowie Steuerelement für ein solches System Expired - Lifetime DE60302861T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0214388 2002-11-18
FR0214388A FR2847352B1 (fr) 2002-11-18 2002-11-18 Systeme de commandes de vol electriques pour aeronef comportant une detection de couplages oscillatoires de pilotage et organe de pilotage pour un tel systeme

Publications (2)

Publication Number Publication Date
DE60302861D1 true DE60302861D1 (de) 2006-01-26
DE60302861T2 DE60302861T2 (de) 2006-08-03

Family

ID=32116638

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60302861T Expired - Lifetime DE60302861T2 (de) 2002-11-18 2003-10-23 System, das eine Anzeigung von Steuerungsschwingungskupplungen verwendet, zur elektrischen Flugsteuerung eines Flugzeugs, sowie Steuerelement für ein solches System

Country Status (6)

Country Link
US (2) US20050021193A1 (de)
EP (1) EP1420320B1 (de)
AT (1) ATE313823T1 (de)
CA (1) CA2447283C (de)
DE (1) DE60302861T2 (de)
FR (1) FR2847352B1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2847353B1 (fr) * 2002-11-18 2006-07-14 Airbus France Procede et dispositif pour la detection de couplages oscillatoires de pilotage dans un aeronef
US7272473B2 (en) * 2004-09-17 2007-09-18 The Boeing Company Methods and systems for analyzing system operator coupling susceptibility
FR2889162B1 (fr) * 2005-07-28 2007-09-07 Airbus France Sas Procede et dispositif de pilotage d'un aeronef selon au moins un axe de pilotage
DE202008005918U1 (de) * 2008-04-29 2009-09-03 Jungheinrich Aktiengesellschaft Betätigungsanordnung für Steuerorgane
FR2980453B1 (fr) * 2011-09-26 2014-06-27 Airbus Operations Sas Systeme electrique de commande de direction pour aeronef
WO2013074134A1 (en) * 2011-11-17 2013-05-23 National Institute Of Aerospace Associates Radiation shielding materials containing hydrogen, boron and nitrogen
JP6433134B2 (ja) 2013-03-19 2018-12-05 株式会社ディ・アンド・ディ 塗布型放射線遮蔽材
US10482783B2 (en) 2015-11-06 2019-11-19 Frasca International, Inc. Adaptive assistance for flight simulation
CN106741870B (zh) * 2016-11-30 2019-03-26 中国直升机设计研究所 一种座舱操纵系统及方法
FR3086273B1 (fr) * 2018-09-26 2020-10-09 Safran Electronics & Defense Dispositif de commande de vol d’un aeronef
CN114044125B (zh) * 2021-12-21 2024-05-14 中国商用飞机有限责任公司 飞行器操纵控制系统及控制方法

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3236478A (en) * 1964-04-23 1966-02-22 North American Aviation Inc Flight control system
US4030011A (en) * 1975-03-24 1977-06-14 Honeywell Inc. Multimode control systems
DE2807902C2 (de) * 1978-02-24 1980-04-30 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Steuereinrichtung mit aktiver Kraft rückführung
US4298833A (en) * 1980-02-29 1981-11-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus for damping operator induced oscillations of a controlled system
US4477043A (en) * 1982-12-15 1984-10-16 The United States Of America As Represented By The Secretary Of The Air Force Biodynamic resistant control stick
DE3431583A1 (de) * 1984-08-28 1986-03-13 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zur automatischen beseitigung von steuerkraftfehlern bei luftfahrzeugen, insbesondere hubschraubern
USH703H (en) * 1987-07-30 1989-11-07 The United States Of America As Represented By The Secretary Of The Air Force Manual control apparatus with electable mechanical impedance
FR2643502B1 (fr) * 1989-02-20 1996-01-19 Aerospatiale Dispositif de commande a manche basculant, notamment pour aeronef, et systeme comportant un tel dispositif
US5076517A (en) * 1989-08-14 1991-12-31 United Technologies Corporation Programmable, linear collective control system for a helicopter
US5107080A (en) * 1989-12-01 1992-04-21 Massachusetts Institute Of Technology Multiple degree of freedom damped hand controls
FR2756392B1 (fr) * 1996-11-22 1999-01-22 Aerospatiale Systeme de couplage de manches de commande
US5935177A (en) * 1997-02-06 1999-08-10 Accurate Automation Corporation Pilot-induced oscillation detection and compensation apparatus and method
US6325331B1 (en) * 1998-12-11 2001-12-04 Bell Helicopter Textron Inc. Trim actuator
US6199028B1 (en) * 1999-02-04 2001-03-06 The United States Of America As Represented By The Secretary Of The Air Force Detector for human loss of tracking control
US6311110B1 (en) * 1999-06-17 2001-10-30 Lord Corporation Adaptive off-state control method
US6459228B1 (en) * 2001-03-22 2002-10-01 Mpc Products Corporation Dual input servo coupled control sticks
US20030183728A1 (en) * 2002-03-29 2003-10-02 The Boeing Company Aircraft control surface controller and associated method
US20040078120A1 (en) * 2002-10-16 2004-04-22 Edgar Melkers Non-linear compensation of a control system having an actuator and a method therefore

Also Published As

Publication number Publication date
ATE313823T1 (de) 2006-01-15
US8473121B2 (en) 2013-06-25
EP1420320A1 (de) 2004-05-19
DE60302861T2 (de) 2006-08-03
EP1420320B1 (de) 2005-12-21
US20100200701A1 (en) 2010-08-12
FR2847352A1 (fr) 2004-05-21
CA2447283C (fr) 2012-04-24
US20050021193A1 (en) 2005-01-27
CA2447283A1 (fr) 2004-05-18
FR2847352B1 (fr) 2005-01-28

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