CN102343976B - 飞机控制系统以及向控制杆提供反馈的方法 - Google Patents

飞机控制系统以及向控制杆提供反馈的方法 Download PDF

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Publication number
CN102343976B
CN102343976B CN201110213940.5A CN201110213940A CN102343976B CN 102343976 B CN102343976 B CN 102343976B CN 201110213940 A CN201110213940 A CN 201110213940A CN 102343976 B CN102343976 B CN 102343976B
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CN
China
Prior art keywords
bar
feedback
respect
centre
mechanical
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 - Fee Related
Application number
CN201110213940.5A
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English (en)
Chinese (zh)
Other versions
CN102343976A (zh
Inventor
Z·P·肖尔伊克
G·P·贾亚拉曼
C·C·弗雷曼
B·P·戴拉
D·S·斯塔赫尼亚克
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Woodward MPC Inc
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Woodward MPC Inc
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.)
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Publication of CN102343976A publication Critical patent/CN102343976A/zh
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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
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/12—Dual control apparatus
    • 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
    • B64C13/503—Fly-by-Wire
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G11/00—Manually-actuated control mechanisms provided with two or more controlling members co-operating with one single controlled member
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G5/00—Means for preventing, limiting or returning the movements of parts of a control mechanism, e.g. locking controlling member
    • G05G5/03—Means for enhancing the operator's awareness of arrival of the controlling member at a command or datum position; Providing feel, e.g. means for creating a counterforce
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G7/00—Manually-actuated control mechanisms provided with one single controlling member co-operating with one single controlled member; Details thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Control Devices (AREA)
  • Transmission Devices (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Control Of Position Or Direction (AREA)
CN201110213940.5A 2010-07-28 2011-07-28 飞机控制系统以及向控制杆提供反馈的方法 Expired - Fee Related CN102343976B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/844,867 2010-07-28
US12/844,867 US8814103B2 (en) 2010-07-28 2010-07-28 Position control system for cross coupled operation of fly-by-wire control columns

Publications (2)

Publication Number Publication Date
CN102343976A CN102343976A (zh) 2012-02-08
CN102343976B true CN102343976B (zh) 2016-05-11

Family

ID=44652350

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201110213940.5A Expired - Fee Related CN102343976B (zh) 2010-07-28 2011-07-28 飞机控制系统以及向控制杆提供反馈的方法

Country Status (7)

Country Link
US (1) US8814103B2 (https=)
JP (1) JP5845017B2 (https=)
CN (1) CN102343976B (https=)
BR (1) BRPI1103504A2 (https=)
DE (1) DE102011052205A1 (https=)
FR (1) FR2963318B1 (https=)
GB (2) GB2501643B (https=)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8770055B2 (en) * 2010-06-11 2014-07-08 Mason Electric Company Multi-axis pivot assembly for control sticks and associated systems and methods
US8814103B2 (en) 2010-07-28 2014-08-26 Woodward Mpc, Inc. Position control system for cross coupled operation of fly-by-wire control columns
US9405312B2 (en) 2010-07-28 2016-08-02 Woodward Mpc, Inc. Active control column with manually activated reversion to passive control column
US9051045B2 (en) 2010-07-28 2015-06-09 Woodward Mpc, Inc. Indirect drive active control column
US8469317B2 (en) * 2010-10-22 2013-06-25 Woodward Mpc, Inc. Line replaceable, fly-by-wire control columns with push-pull interconnect rods
US8729848B2 (en) 2010-12-22 2014-05-20 Woodward Mpc Inc. Fail-passive variable gradient control stick drive system
US9126676B2 (en) 2011-10-28 2015-09-08 Woodward Mpc, Inc. Compact two axis gimbal for control stick
JP5819780B2 (ja) * 2012-05-30 2015-11-24 住友精密工業株式会社 航空機操向装置の制御装置
FR2993065B1 (fr) * 2012-07-09 2014-08-29 Ratier Figeac Soc Dispositif de conjugaison d'effort entre organes de pilotage, organe de pilotage et aeronef
GB201220653D0 (en) * 2012-11-16 2013-01-02 Mcculloch Norman L Improvements in aircraft
WO2014199212A1 (en) * 2013-06-14 2014-12-18 Bombardier Inc. Aircraft sidestick priority and dual input control logic
FR3012112B1 (fr) * 2013-10-22 2017-04-21 Ratier Figeac Soc Procede de surveillance de fonctionnement d'un dispositif de pilotage d'aeronef et dispositif de pilotage d'aeronef ainsi surveille
CN103600836B (zh) * 2013-11-08 2015-08-05 中航飞机股份有限公司西安飞机分公司 一种飞机突风锁防误操作结构
CN103744289B (zh) * 2013-12-27 2017-05-03 李竞捷 电传飞机双重输入选择性执行控制方法
CN106184713B (zh) * 2015-04-29 2018-07-24 陕西飞机工业（集团）有限公司 一种飞机升降舵调整片自动配平方法
FR3038294B1 (fr) * 2015-06-30 2018-04-06 Airbus Helicopters Procede de commande des moyen aerodynamiques d'un aeronef, systeme de commande associe et aeronef equipe d'un tel systeme de commande
FR3058806B1 (fr) * 2016-11-14 2019-01-25 Dassault Aviation Dispositif de gestion de l'energie mecanique d'un aeronef, presentant un systeme d'application de force sur une manette de commande, aeronef et procede associes
US10074245B2 (en) 2017-01-10 2018-09-11 Woodward, Inc. Force feel using a brushless DC motor
GB2577720B (en) * 2018-10-04 2023-04-19 Bae Systems Plc Oscilation system
US11396362B2 (en) 2019-11-01 2022-07-26 Woodward, Inc. Rudder and brake pedal assembly
FR3117624B1 (fr) 2020-12-15 2022-12-16 Dassault Aviat Dispositif de pilotage d'un aéronef et procédé associé
FR3117623A1 (fr) * 2020-12-15 2022-06-17 Dassault Aviation Dispositif de pilotage d'un aéronef et procédé associé
GB2618154B (en) * 2022-04-29 2025-01-22 Bae Systems Plc A control unit in an active inceptor
JP2025514973A (ja) * 2022-04-29 2025-05-13 ビ－エイイ－ システムズ パブリック リミテッド カンパニ－ アクティブインセプタ内の制御ユニット
EP4269235A1 (en) * 2022-04-29 2023-11-01 BAE SYSTEMS plc A control unit in an active inceptor
WO2025116487A1 (en) * 2023-11-28 2025-06-05 Hyundai Motor Company Method for flight control based on flight abnormal conditions and air mobility apparatus using the same

Family Cites Families (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB126568A (en) 1918-10-08 1919-05-15 James Frederick Verner Improvements in Aeroplane Controls.
US2060806A (en) * 1932-12-14 1936-11-17 Hunt Mabel Graybill Aircraft intercommunication system
US2833496A (en) * 1954-12-13 1958-05-06 Northrop Aircraft Inc Flight control system
GB827089A (en) 1955-03-03 1960-02-03 Honeywell Regulator Co Improvements in control systems for dirigible craft
GB925471A (en) 1959-08-31 1963-05-08 William Warren Triggs C B E Manual and automatic hydraulic servomechanism
US3776058A (en) 1972-05-17 1973-12-04 Us Navy Multi-axis hand controller
US3902379A (en) 1973-12-03 1975-09-02 Us Navy High load, quick-disconnect link
FR2525000A1 (fr) 1982-04-07 1983-10-14 Aerospatiale Manche de commande debrayable pour copilote d'aeronef
US4422851A (en) 1982-05-12 1983-12-27 The United States Of America As Represented By The Secretary Of The Navy isometric grip bending beam control
FR2558136B1 (fr) 1984-01-12 1986-04-25 Aerospatiale Dispositif de commande pourvu de deux manches conjugues et actionnes respectivement par une main gauche et par une main droite
JPS6133126U (ja) * 1984-07-30 1986-02-28 愛知機械工業株式会社 変速操作部のセレクトリタ−ン構造
US4716399A (en) 1985-01-14 1987-12-29 The Boeing Company Optomechanical control apparatus
FR2583017B1 (fr) 1985-06-07 1987-09-18 Aerospatiale Dispositif de commande pourvu de deux manches couples
US4717098A (en) 1986-05-19 1988-01-05 Mcdonnell Douglas Corporation Actuator for a g-limiter override
US4980835A (en) * 1988-10-13 1990-12-25 United Technologies Corporation Control law system for X-Wing aircraft
US5107080A (en) 1989-12-01 1992-04-21 Massachusetts Institute Of Technology Multiple degree of freedom damped hand controls
US5149023A (en) 1991-07-12 1992-09-22 The Boeing Company Mechanically-linked side stick controllers with isolated pitch and roll control movement
US5291113A (en) 1992-10-06 1994-03-01 Honeywell Inc. Servo coupled hand controllers
US5456428A (en) 1993-07-21 1995-10-10 Honeywell Inc. Mechanically linked active sidesticks
FR2728537A1 (fr) 1994-12-21 1996-06-28 Eurocopter France Dispositif pour l'actionnement d'un organe commande pour un aeronef, tel que notamment un helicoptere, a commandes de vol electriques
US5694014A (en) * 1995-08-22 1997-12-02 Honeywell Inc. Active hand controller redundancy and architecture
US7027032B2 (en) * 1995-12-01 2006-04-11 Immersion Corporation Designing force sensations for force feedback computer applications
FR2756392B1 (fr) 1996-11-22 1999-01-22 Aerospatiale Systeme de couplage de manches de commande
US6572055B1 (en) 1999-08-10 2003-06-03 Bombardier Aerospace Corporation Hydrostatic sidestick coupling
US20040026158A1 (en) * 2000-03-27 2004-02-12 Peter Rieth Vehicle system and axle guide module for a vehicle steering system
US6459228B1 (en) * 2001-03-22 2002-10-01 Mpc Products Corporation Dual input servo coupled control sticks
WO2003040844A2 (en) * 2001-11-06 2003-05-15 Bombardier Inc. Apparatus for controlling a joystick having force-feedback
CA2497228A1 (en) * 2002-08-29 2004-03-11 Dept. Of Veterans Affairs Variable compliance joystick with compensation algorithms
FR2888009B1 (fr) * 2005-06-30 2007-09-07 Dassault Aviat Dispositif de commande comportant deux manches couples pour permettre de placer des organes commandes dans des positions souhaitees
JP2009523657A (ja) * 2006-01-17 2009-06-25 ガルフストリーム・エアロスペース・コーポレイション 統合バックアップ制御システム用のシステムおよび方法
US7759894B2 (en) * 2006-10-26 2010-07-20 Honeywell International Inc. Cogless motor driven active user interface haptic feedback system
US7658349B2 (en) 2006-10-26 2010-02-09 Honeywell International Inc. Pilot flight control stick haptic feedback system and method
US20080156939A1 (en) * 2007-01-03 2008-07-03 Honeywell International, Inc. Active pilot flight control stick system with passive electromagnetic feedback
JP4772712B2 (ja) 2007-02-19 2011-09-14 本田技研工業株式会社 車両のペダル式操作装置
US20110148666A1 (en) * 2007-04-04 2011-06-23 Honeywell International, Inc. User interface passive haptic feedback system
US8002220B2 (en) * 2007-10-25 2011-08-23 Honeywell International Inc. Rate limited active pilot inceptor system and method
GB2465761A (en) 2008-11-27 2010-06-02 Gm Global Tech Operations Inc A clutch pedal with a spring having an adjustable spring characteristic
US8814103B2 (en) 2010-07-28 2014-08-26 Woodward Mpc, Inc. Position control system for cross coupled operation of fly-by-wire control columns
US8469317B2 (en) * 2010-10-22 2013-06-25 Woodward Mpc, Inc. Line replaceable, fly-by-wire control columns with push-pull interconnect rods
US8729848B2 (en) * 2010-12-22 2014-05-20 Woodward Mpc Inc. Fail-passive variable gradient control stick drive system

Also Published As

Publication number Publication date
DE102011052205A9 (de) 2012-05-16
GB2482407B (en) 2013-09-25
GB2482407A (en) 2012-02-01
GB201112853D0 (en) 2011-09-07
DE102011052205A1 (de) 2012-02-02
FR2963318B1 (fr) 2017-06-23
JP2012030791A (ja) 2012-02-16
GB2501643B (en) 2014-05-07
FR2963318A1 (fr) 2012-02-03
BRPI1103504A2 (pt) 2015-07-28
CN102343976A (zh) 2012-02-08
US20120025029A1 (en) 2012-02-02
US8814103B2 (en) 2014-08-26
GB2501643A (en) 2013-10-30
JP5845017B2 (ja) 2016-01-20
GB201313574D0 (en) 2013-09-11

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160511

Termination date: 20200728

CF01 Termination of patent right due to non-payment of annual fee