IL86127A0 - Flight control system employing three controllers operating a dual actuator - Google Patents

Flight control system employing three controllers operating a dual actuator

Info

Publication number
IL86127A0
IL86127A0 IL86127A IL8612788A IL86127A0 IL 86127 A0 IL86127 A0 IL 86127A0 IL 86127 A IL86127 A IL 86127A IL 8612788 A IL8612788 A IL 8612788A IL 86127 A0 IL86127 A0 IL 86127A0
Authority
IL
Israel
Prior art keywords
control system
flight control
system employing
dual actuator
controllers operating
Prior art date
Application number
IL86127A
Other languages
English (en)
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of IL86127A0 publication Critical patent/IL86127A0/xx

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
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
    • 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
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Safety Devices In Control Systems (AREA)
  • Servomotors (AREA)
IL86127A 1987-04-23 1988-04-19 Flight control system employing three controllers operating a dual actuator IL86127A0 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/041,872 US4807516A (en) 1987-04-23 1987-04-23 Flight control system employing three controllers operating a dual actuator

Publications (1)

Publication Number Publication Date
IL86127A0 true IL86127A0 (en) 1988-11-15

Family

ID=21918795

Family Applications (1)

Application Number Title Priority Date Filing Date
IL86127A IL86127A0 (en) 1987-04-23 1988-04-19 Flight control system employing three controllers operating a dual actuator

Country Status (6)

Country Link
US (1) US4807516A (xx)
EP (1) EP0288034A3 (xx)
JP (1) JPS6460497A (xx)
CN (1) CN88102523A (xx)
BR (1) BR8801907A (xx)
IL (1) IL86127A0 (xx)

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US7689383B2 (en) * 2003-11-20 2010-03-30 The Boeing Company Component health assessment for reconfigurable control
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US20100318245A1 (en) * 2005-03-03 2010-12-16 Nabtesco Corporation Flight control system
US7789345B2 (en) * 2005-03-03 2010-09-07 Nabtesco Corporation Actuator control apparatus
DE102005042511A1 (de) * 2005-09-07 2007-04-05 Airbus Deutschland Gmbh Trimmaktuator-Betätigungssystem für einen hydraulisch betätigbaren Trimmable Horizontal Stabilizer Actuator
JP2009523658A (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 分散型飛行制御システムのバックアップ制御のための装置及び方法
BRPI0706593A2 (pt) * 2006-01-17 2011-04-05 Gulfstream Aerospace Corp sistema e método para um sistema de controle de backup integrado
US7424642B2 (en) * 2006-04-24 2008-09-09 Gm Global Technology Operations, Inc. Method for synchronization of a controller
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CA2683132C (en) 2007-04-05 2013-10-29 Bombardier Inc. Multi-axis serially redundant, single channel, multi-path fly-by-wire flight control system
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US8955365B2 (en) * 2008-12-23 2015-02-17 Embraer S.A. Performance monitoring and prognostics for aircraft pneumatic control valves
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US8594852B2 (en) * 2010-02-22 2013-11-26 Eaton Corporation Device and method for controlling a fluid actuator
JP5590955B2 (ja) 2010-04-26 2014-09-17 ナブテスコ株式会社 アクチュエータ制御システム
US8534599B2 (en) 2011-03-31 2013-09-17 Hamilton Sundstrand Corporation Redundant two stage electro-hydraulic servo actuator control
US8620522B2 (en) 2011-05-25 2013-12-31 The Boeing Company Suppressing electrical failure effects in servo control systems
US9625894B2 (en) * 2011-09-22 2017-04-18 Hamilton Sundstrand Corporation Multi-channel control switchover logic
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CN102662383B (zh) * 2012-05-29 2014-11-19 张二浩 用于控制链条系统的控制链条实现方法
JP6178587B2 (ja) * 2013-02-28 2017-08-09 三菱航空機株式会社 航空機のアクチュエータ装置、及び、航空機
FR3009581B1 (fr) * 2013-08-09 2015-09-25 Snecma Procede de surveillance d'une vanne d'un moteur d'aeronef
BR112016007465B1 (pt) * 2013-10-03 2021-12-21 Transocean Innovation Labs Ltd Aparelhos hidráulicos e processo de atuação dos mesmos
KR101530181B1 (ko) * 2014-12-09 2015-06-22 국방과학연구소 가상 제어 구조를 갖는 다중화 구동 제어시스템
US9563523B2 (en) * 2015-04-16 2017-02-07 GM Global Technology Operations LLC Architecture for scalable fault tolerance in integrated fail-silent and fail-operational systems
CN112083712A (zh) 2016-02-29 2020-12-15 深圳市大疆创新科技有限公司 油门控制信号处理方法、电子调速器、控制器及移动平台
CN106774367B (zh) * 2016-12-27 2020-05-15 歌尔股份有限公司 一种飞行器的冗余控制方法
US10759520B2 (en) 2017-09-29 2020-09-01 The Boeing Company Flight control system and method of use
CN109407631B (zh) * 2018-09-29 2020-09-22 珠海格力电器股份有限公司 输入负载信息的处理方法、装置、机组和存储介质
CN109991841B (zh) * 2019-03-27 2022-04-05 西安联飞智能装备研究院有限责任公司 飞行控制计算系统及控制信号输出方法、装置和存储介质
JP6772341B2 (ja) * 2019-07-01 2020-10-21 トランスオーシャン イノベーション ラブス リミテッド 液圧デバイスおよびそれを作動する方法
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Also Published As

Publication number Publication date
US4807516A (en) 1989-02-28
BR8801907A (pt) 1988-11-22
JPS6460497A (en) 1989-03-07
EP0288034A2 (en) 1988-10-26
CN88102523A (zh) 1988-11-02
EP0288034A3 (en) 1990-01-17

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