FR2756252B1 - Systeme de commande de vol pour aeronef a voilure tournante, notamment pour un helicoptere - Google Patents

Systeme de commande de vol pour aeronef a voilure tournante, notamment pour un helicoptere

Info

Publication number
FR2756252B1
FR2756252B1 FR9614288A FR9614288A FR2756252B1 FR 2756252 B1 FR2756252 B1 FR 2756252B1 FR 9614288 A FR9614288 A FR 9614288A FR 9614288 A FR9614288 A FR 9614288A FR 2756252 B1 FR2756252 B1 FR 2756252B1
Authority
FR
France
Prior art keywords
aircraft
helicopter
control system
flight control
rotating
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
FR9614288A
Other languages
English (en)
Other versions
FR2756252A1 (fr
Inventor
Jacques Serge Louis Bellera
Serge Joseph Mezan
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 Helicopters SAS
Original Assignee
Eurocopter France SA
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 Eurocopter France SA filed Critical Eurocopter France SA
Priority to FR9614288A priority Critical patent/FR2756252B1/fr
Priority to US08/976,502 priority patent/US6070829A/en
Publication of FR2756252A1 publication Critical patent/FR2756252A1/fr
Application granted granted Critical
Publication of FR2756252B1 publication Critical patent/FR2756252B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
    • 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
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B64C13/22—Initiating means actuated automatically, e.g. responsive to gust detectors readily revertible to personal control

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)
  • Toys (AREA)
FR9614288A 1996-11-22 1996-11-22 Systeme de commande de vol pour aeronef a voilure tournante, notamment pour un helicoptere Expired - Fee Related FR2756252B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR9614288A FR2756252B1 (fr) 1996-11-22 1996-11-22 Systeme de commande de vol pour aeronef a voilure tournante, notamment pour un helicoptere
US08/976,502 US6070829A (en) 1996-11-22 1997-11-24 Flight control system for rotary-wing aircraft, especially for a helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9614288A FR2756252B1 (fr) 1996-11-22 1996-11-22 Systeme de commande de vol pour aeronef a voilure tournante, notamment pour un helicoptere

Publications (2)

Publication Number Publication Date
FR2756252A1 FR2756252A1 (fr) 1998-05-29
FR2756252B1 true FR2756252B1 (fr) 1999-01-22

Family

ID=9497907

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9614288A Expired - Fee Related FR2756252B1 (fr) 1996-11-22 1996-11-22 Systeme de commande de vol pour aeronef a voilure tournante, notamment pour un helicoptere

Country Status (2)

Country Link
US (1) US6070829A (fr)
FR (1) FR2756252B1 (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1306612B1 (it) * 1998-11-11 2001-06-18 Marco Testi Metodo di interfaccia tra un pilota e le superfici di un aeromobile,attrezzatura di interfaccia per attuare tale metodo e sensori dello
FR2802656B1 (fr) * 1999-12-16 2002-02-15 Eurocopter France Systeme de commande de vol pour aeronef a voilure tournante, notamment pour helicoptere
US6561463B1 (en) 2000-07-14 2003-05-13 Honeywell International Inc. Flight control module with integrated spoiler actuator control electronics
FR2832123B1 (fr) 2001-11-14 2004-10-29 Eurocopter France Systeme de commande de vol, pour commander le tangage d'un aeronef a decollage vertical et a direction de portance orientable
US20050136666A1 (en) * 2003-12-23 2005-06-23 Tokyo Electron Limited Method and apparatus for etching an organic layer
US7438259B1 (en) * 2006-08-16 2008-10-21 Piasecki Aircraft Corporation Compound aircraft control system and method
CA2824932C (fr) 2011-01-14 2016-03-22 Bell Helicopter Textron Inc. Lois de commande de vol pour commande de trajectoire de vol vertical
EP2732351B1 (fr) * 2011-07-12 2015-09-02 Bell Helicopter Textron Inc. Affichage de marge de contrôle cyclique de pilotage
FR3023016B1 (fr) 2014-06-30 2016-07-01 Airbus Helicopters Systeme et procede de commande de vol en tenue de trajectoire pour un aeronef a voilure tournante
FR3023017B1 (fr) 2014-06-30 2016-06-10 Airbus Helicopters Systeme et procede de commande de vol d'un aeronef a voilure tournante en tenue de trajectoire ou tenue de cap selon sa vitesse d'avancement
FR3023018B1 (fr) 2014-06-30 2016-06-10 Airbus Helicopters Procede et systeme de mise en vol stationnaire d'un aeronef a voilure tournante en tenue de trajectoire ou tenue de cap selon sa vitesse d'avancement
TWI642596B (zh) * 2016-01-18 2018-12-01 緯創資通股份有限公司 任意角度空拋的多軸無人飛行載具的平衡控制方法、其電腦程式產品及其多軸無人飛行載具

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3520499A (en) * 1968-05-29 1970-07-14 United Aircraft Corp Flight control system
US3626163A (en) * 1970-01-28 1971-12-07 Us Army Automatic landing system
CA1050633A (fr) * 1974-12-19 1979-03-13 Ronald J. Miller Systeme semi-automatique de controle de vol utilisant un dispositif de stabilisation a autorite limitee
US4387430A (en) * 1981-03-30 1983-06-07 United Technologies Corporation Pitch stick force inhibit of aircraft automatic outer loop
US4527242A (en) * 1982-06-28 1985-07-02 Rockwell International Corporation Automatic flight control pilot assist system
US4642774A (en) * 1982-07-01 1987-02-10 Rockwell International Corporation Automatic flight control with pilot fly-through
US5255880A (en) * 1991-02-08 1993-10-26 Rockwell International Corporation Fly by wire/fly by light control system with manual override
US5224664A (en) * 1991-07-22 1993-07-06 United Technologies Corporation Adaptive control system input limiting
US5641136A (en) * 1994-12-22 1997-06-24 Eidetics Aircraft, Inc. Combat agility management system

Also Published As

Publication number Publication date
US6070829A (en) 2000-06-06
FR2756252A1 (fr) 1998-05-29

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20150731