FR2686310B1 - Systeme pour la commande d'une surface aerodynamique d'un aeronef. - Google Patents

Systeme pour la commande d'une surface aerodynamique d'un aeronef.

Info

Publication number
FR2686310B1
FR2686310B1 FR9200529A FR9200529A FR2686310B1 FR 2686310 B1 FR2686310 B1 FR 2686310B1 FR 9200529 A FR9200529 A FR 9200529A FR 9200529 A FR9200529 A FR 9200529A FR 2686310 B1 FR2686310 B1 FR 2686310B1
Authority
FR
France
Prior art keywords
aircraft
controlling
aerodynamic surface
aerodynamic
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
FR9200529A
Other languages
English (en)
Other versions
FR2686310A1 (fr
Inventor
Pascal Traverse
Tron Xavier Le
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 Group SAS
Original Assignee
Airbus Group 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 Group SAS filed Critical Airbus Group SAS
Priority to FR9200529A priority Critical patent/FR2686310B1/fr
Priority to US07/994,907 priority patent/US5374014A/en
Publication of FR2686310A1 publication Critical patent/FR2686310A1/fr
Application granted granted Critical
Publication of FR2686310B1 publication Critical patent/FR2686310B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B64C13/503—Fly-by-Wire
    • 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
    • G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa

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)
  • Feedback Control In General (AREA)
FR9200529A 1992-01-20 1992-01-20 Systeme pour la commande d'une surface aerodynamique d'un aeronef. Expired - Lifetime FR2686310B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR9200529A FR2686310B1 (fr) 1992-01-20 1992-01-20 Systeme pour la commande d'une surface aerodynamique d'un aeronef.
US07/994,907 US5374014A (en) 1992-01-20 1992-12-22 System for control of an aerodynamic surface of an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9200529A FR2686310B1 (fr) 1992-01-20 1992-01-20 Systeme pour la commande d'une surface aerodynamique d'un aeronef.

Publications (2)

Publication Number Publication Date
FR2686310A1 FR2686310A1 (fr) 1993-07-23
FR2686310B1 true FR2686310B1 (fr) 1994-04-08

Family

ID=9425773

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9200529A Expired - Lifetime FR2686310B1 (fr) 1992-01-20 1992-01-20 Systeme pour la commande d'une surface aerodynamique d'un aeronef.

Country Status (2)

Country Link
US (1) US5374014A (fr)
FR (1) FR2686310B1 (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0408498B1 (fr) * 1989-07-13 1994-09-14 Ciba-Geigy Ag Pigments à effets organiques en paillettes
US5806805A (en) * 1996-08-07 1998-09-15 The Boeing Company Fault tolerant actuation system for flight control actuators
FR2778164B1 (fr) * 1998-04-29 2000-06-23 Aerospatiale Systeme de commande mixte pour surface aerodynamique d'aeronef
US6366837B1 (en) 2000-07-14 2002-04-02 Honeywell International Inc. Method for providing command augmentation to a command lane within a vehicle
US6443399B1 (en) 2000-07-14 2002-09-03 Honeywell International Inc. Flight control module merged into the integrated modular avionics
US6561463B1 (en) 2000-07-14 2003-05-13 Honeywell International Inc. Flight control module with integrated spoiler actuator control electronics
US6446911B1 (en) 2000-07-14 2002-09-10 Honeywell International Inc. Method for controlling actuators on a vehicle
US6578425B2 (en) 2001-05-29 2003-06-17 Honeywell Inc. Apparatus and method for verifying the dynamic stiffness capability of hydraulic servo actuators
JP4490963B2 (ja) 2003-02-15 2010-06-30 ガルフストリーム・エアロスペース・コーポレイション 航空機キャビン大気組成制御方法
FR2882141B1 (fr) * 2005-02-14 2007-05-04 Airbus France Sas Procede et dispositif pour detecter au sol l'obstruction d'une prise de pression d'un capteur de pression statique d'un aeronef
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
EP1977297A4 (fr) * 2006-01-17 2010-02-24 Gulfstream Aerospace Corp Appareil et procédé de commande de secours utilisés dans un système de commande de vol distribué
FR2932625B1 (fr) * 2008-06-16 2010-05-28 Airbus France Dispositif de comptage d'oscillations d'un signal temporel oscillant
CN104554711B (zh) * 2014-09-12 2017-05-17 北京精密机电控制设备研究所 用于控制飞行器空气舵负载摆角的空气动力控制伺服***

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB800958A (en) * 1955-06-10 1958-09-03 Sperry Rand Corp Fluid pressure artificial spring devices
US3027878A (en) * 1959-06-10 1962-04-03 Honeywell Regulator Co Fluid motor control apparatus
US3221229A (en) * 1962-01-22 1965-11-30 Massachusetts Inst Technology Model reference adaptive control system
US4019697A (en) * 1975-08-25 1977-04-26 The Garrett Corporation Fluidic approach power compensator control system
DE2615345C3 (de) * 1976-04-08 1984-05-10 Liebherr-Aero-Technik Gmbh, 8998 Lindenberg Selbstüberwachter Stellantrieb, insbesondere für Steuerruder von Flugzeugen
US4826110A (en) * 1987-06-22 1989-05-02 The Boeing Company Oscillatory failure monitor
US4913032A (en) * 1988-12-19 1990-04-03 Woodward Governor Company Multiplexed hydraulic control systems
SU1744001A1 (ru) * 1990-02-19 1992-06-30 Молодежный Центр "Союз" Система управлени рулевыми органами летательного аппарата
JP2879946B2 (ja) * 1990-06-04 1999-04-05 帝人製機株式会社 航空機翼のフラッタ抑制システム

Also Published As

Publication number Publication date
FR2686310A1 (fr) 1993-07-23
US5374014A (en) 1994-12-20

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Legal Events

Date Code Title Description
CD Change of name or company name
TP Transmission of property