FR2814433B1 - Dispositif de commande de vol d'un aeronef, en particulier d'un helicoptere - Google Patents

Dispositif de commande de vol d'un aeronef, en particulier d'un helicoptere

Info

Publication number
FR2814433B1
FR2814433B1 FR0012345A FR0012345A FR2814433B1 FR 2814433 B1 FR2814433 B1 FR 2814433B1 FR 0012345 A FR0012345 A FR 0012345A FR 0012345 A FR0012345 A FR 0012345A FR 2814433 B1 FR2814433 B1 FR 2814433B1
Authority
FR
France
Prior art keywords
helicopter
flight
aircraft
controlling
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
FR0012345A
Other languages
English (en)
Other versions
FR2814433A1 (fr
Inventor
Serge 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
Eurocopter 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, Eurocopter SA filed Critical Eurocopter France SA
Priority to FR0012345A priority Critical patent/FR2814433B1/fr
Priority to US09/963,797 priority patent/US6622065B2/en
Publication of FR2814433A1 publication Critical patent/FR2814433A1/fr
Application granted granted Critical
Publication of FR2814433B1 publication Critical patent/FR2814433B1/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
    • G05D1/08—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

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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
FR0012345A 2000-09-28 2000-09-28 Dispositif de commande de vol d'un aeronef, en particulier d'un helicoptere Expired - Lifetime FR2814433B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0012345A FR2814433B1 (fr) 2000-09-28 2000-09-28 Dispositif de commande de vol d'un aeronef, en particulier d'un helicoptere
US09/963,797 US6622065B2 (en) 2000-09-28 2001-09-27 Flight control device for an aircraft, in particular for a helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0012345A FR2814433B1 (fr) 2000-09-28 2000-09-28 Dispositif de commande de vol d'un aeronef, en particulier d'un helicoptere

Publications (2)

Publication Number Publication Date
FR2814433A1 FR2814433A1 (fr) 2002-03-29
FR2814433B1 true FR2814433B1 (fr) 2002-12-13

Family

ID=8854768

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0012345A Expired - Lifetime FR2814433B1 (fr) 2000-09-28 2000-09-28 Dispositif de commande de vol d'un aeronef, en particulier d'un helicoptere

Country Status (2)

Country Link
US (1) US6622065B2 (fr)
FR (1) FR2814433B1 (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7463956B2 (en) * 2003-07-03 2008-12-09 The Boeing Company Constant vertical state maintaining cueing system
EP2261116B1 (fr) * 2009-06-09 2019-05-22 Sikorsky Aircraft Corporation Système de compensation automatique pour avion à commandes électriques avec contrôleurs de compensation uniques
WO2011072362A1 (fr) * 2009-12-18 2011-06-23 National Research Council Of Canada Mode de réponse pour système de commande d'embarcation pilotée
US9304516B2 (en) 2011-01-14 2016-04-05 Textron Innovations Inc. Flight control laws for vertical flight path
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
FR3030760B1 (fr) 2014-12-18 2017-12-22 Airbus Helicopters Procede et systeme de determination d'une vitesse angulaire en virage pour un aeronef a voilure tournante
FR3036805B1 (fr) 2015-05-28 2018-06-29 Airbus Helicopters Procede de determination de la vitesse air longitudinale et de la vitesse sol longitudinale d'un aeronef a voiture tournante selon son exposition au vent
FR3044634B1 (fr) 2015-12-08 2017-12-22 Airbus Helicopters Procede et dispositif de pilotage d'un aeronef
US11067981B2 (en) * 2017-03-01 2021-07-20 Textron Innovations, Inc. Aircraft control mode transition smoothing
US11299259B2 (en) * 2020-01-29 2022-04-12 Textron Innovations Inc. Hybrid low speed control

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5213282A (en) * 1991-08-28 1993-05-25 United Technologies Corporation Maneuver feel system for a rotary wing aircraft
US5446666A (en) * 1994-05-17 1995-08-29 The Boeing Company Ground state-fly state transition control for unique-trim aircraft flight control system
US5596499A (en) * 1995-02-21 1997-01-21 The Boeing Company Control law mode switching between rate command and attitude command control systems
US5931421A (en) * 1995-08-11 1999-08-03 Daimler-Benz Aerospace Ag Arrangement for attitude control and stabilization of a three axes stabilized spacecraft
JP3195918B2 (ja) * 1999-03-12 2001-08-06 株式会社コミュータヘリコプタ先進技術研究所 ヘリコプタ用飛行制御装置
JP4709390B2 (ja) * 1999-03-15 2011-06-22 デカ・プロダクツ・リミテッド・パートナーシップ バランスをとる個人用乗物の制御

Also Published As

Publication number Publication date
US20020052675A1 (en) 2002-05-02
FR2814433A1 (fr) 2002-03-29
US6622065B2 (en) 2003-09-16

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Legal Events

Date Code Title Description
CL Concession to grant licences
CD Change of name or company name

Owner name: AIRBUS HELICOPTERS, FR

Effective date: 20140602

PLFP Fee payment

Year of fee payment: 17

PLFP Fee payment

Year of fee payment: 18