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)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (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 (fr)
EP (1) EP0288034A3 (fr)
JP (1) JPS6460497A (fr)
CN (1) CN88102523A (fr)
BR (1) BR8801907A (fr)
IL (1) IL86127A0 (fr)

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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
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CA2637226A1 (fr) * 2006-01-17 2007-07-26 Gulfstream Aerospace Corporation Appareil et procede de commande de secours utilises dans un systeme de commande de vol distribue
US7424642B2 (en) * 2006-04-24 2008-09-09 Gm Global Technology Operations, Inc. Method for synchronization of a controller
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US8955365B2 (en) * 2008-12-23 2015-02-17 Embraer S.A. Performance monitoring and prognostics for aircraft pneumatic control valves
FR2941551B1 (fr) 2009-01-28 2011-06-03 Airbus France Circuit electronique de determination d'une donnee representative d'un parametre de l'air et systeme comprenant un tel circuit
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
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US9625894B2 (en) * 2011-09-22 2017-04-18 Hamilton Sundstrand Corporation Multi-channel control switchover logic
CN103303466B (zh) * 2012-03-09 2016-03-30 陕西飞机工业（集团）有限公司 一种飞机舵面锁防差错电气控制方法及其系统
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
KR102297588B1 (ko) * 2013-10-03 2021-09-07 트랜스오션 이노베이션 랩스 리미티드 유압 디바이스 및 그 작동 방법
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
EP3812279B1 (fr) 2016-02-29 2022-04-13 SZ DJI Technology Co., Ltd. Procédé de traitement de signal de commande d'accélération et régulateur de vitesse électronique
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
JPS6460497A (en) 1989-03-07
EP0288034A3 (fr) 1990-01-17
CN88102523A (zh) 1988-11-02
EP0288034A2 (fr) 1988-10-26
US4807516A (en) 1989-02-28
BR8801907A (pt) 1988-11-22

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