FR3024126B1 - Systeme de controle d'un aeronef - Google Patents

Systeme de controle d'un aeronef Download PDF

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Publication number
FR3024126B1
FR3024126B1 FR1457178A FR1457178A FR3024126B1 FR 3024126 B1 FR3024126 B1 FR 3024126B1 FR 1457178 A FR1457178 A FR 1457178A FR 1457178 A FR1457178 A FR 1457178A FR 3024126 B1 FR3024126 B1 FR 3024126B1
Authority
FR
France
Prior art keywords
aircraft
mode
control system
selection member
operate according
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.)
Active
Application number
FR1457178A
Other languages
English (en)
Other versions
FR3024126A1 (fr
Inventor
Pierre Scacchi
Thierry Bourret
Franck Laine
Matthieu MAYOLLE
Sabrina BETTON
Cecile Puissacq
Olivier Sapin
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 Operations SAS
Original Assignee
Airbus Operations 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 Operations SAS filed Critical Airbus Operations SAS
Priority to FR1457178A priority Critical patent/FR3024126B1/fr
Priority to US14/808,453 priority patent/US9994303B2/en
Publication of FR3024126A1 publication Critical patent/FR3024126A1/fr
Application granted granted Critical
Publication of FR3024126B1 publication Critical patent/FR3024126B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B64C13/02—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
    • 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
    • B64C13/04—Initiating means actuated personally
    • B64C13/042—Initiating means actuated personally operated by hand
    • 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
    • B64C13/04—Initiating means actuated personally
    • B64C13/042—Initiating means actuated personally operated by hand
    • B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
    • 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
    • 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
    • B64C13/18—Initiating means actuated automatically, e.g. responsive to gust detectors using automatic pilot
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
    • G01C23/005—Flight directors

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)

Abstract

L'invention a pour objet un système de contrôle (1) d'un aéronef configuré pour fonctionner selon un premier mode de fonctionnement correspondant à un pilotage automatique de l'aéronef et un deuxième mode de fonctionnement correspondant à un pilotage manuel de l'aéronef, le système comportant un organe de sélection (11). Selon l'invention, le système est configuré pour fonctionner selon le premier mode de fonctionnement lorsque l'organe de sélection (11) délivre un signal d'état inactif et pour fonctionner selon le deuxième mode de fonctionnement lorsque l'organe de sélection délivre un signal d'état actif.
FR1457178A 2014-07-25 2014-07-25 Systeme de controle d'un aeronef Active FR3024126B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1457178A FR3024126B1 (fr) 2014-07-25 2014-07-25 Systeme de controle d'un aeronef
US14/808,453 US9994303B2 (en) 2014-07-25 2015-07-24 Control system and method for an aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1457178 2014-07-25
FR1457178A FR3024126B1 (fr) 2014-07-25 2014-07-25 Systeme de controle d'un aeronef

Publications (2)

Publication Number Publication Date
FR3024126A1 FR3024126A1 (fr) 2016-01-29
FR3024126B1 true FR3024126B1 (fr) 2019-05-17

Family

ID=51894135

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1457178A Active FR3024126B1 (fr) 2014-07-25 2014-07-25 Systeme de controle d'un aeronef

Country Status (2)

Country Link
US (1) US9994303B2 (fr)
FR (1) FR3024126B1 (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11299257B2 (en) * 2014-10-13 2022-04-12 Gulfstream Aerospace Corporation Aircraft, systems, and methods for trim control in fly-by-wire aircraft systems
FR3046262B1 (fr) * 2015-12-24 2018-06-15 Dassault Aviation Systeme et procede de commande et de surveillance d'equipements d'un aeronef
DE102017104903A1 (de) * 2016-03-08 2017-09-14 Gulfstream Aerospace Corporation Rekonfigurierbare Flugleitpanele für ein Luftfahrzeug der Transportkategorie
WO2018161287A1 (fr) * 2017-03-09 2018-09-13 SZ DJI Technology Co., Ltd. Systèmes et procédés permettant de faire fonctionner un véhicule aérien sans pilote
US10870482B2 (en) 2018-04-13 2020-12-22 Hamilton Sunstrand Corporation Aircraft control selector levers
US11091274B2 (en) 2018-05-11 2021-08-17 Gulfstream Aerospace Corporation Aircraft flight guidance panels with integrated standby displays
US11440675B2 (en) 2018-05-21 2022-09-13 Gulfstream Aerospace Corporation Aircraft flight guidance panels with a display disposed between two input portions
CN108803641B (zh) * 2018-06-08 2022-08-05 深圳臻迪信息技术有限公司 飞行控制方法及飞行器
SG11202106279TA (en) * 2018-12-19 2021-07-29 Safran Electronics & Defense Method for piloting an aircraft
US11649066B2 (en) * 2019-08-06 2023-05-16 Gulfstream Aerospace Corporation Flight guidance panels with joystick controls
CN111930136B (zh) * 2020-08-21 2022-07-12 中国工程物理研究院总体工程研究所 一种飞行调参的工程方法

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3337163A (en) * 1965-05-10 1967-08-22 Brittan Ind Inc Aircraft touch control system
US5797564A (en) * 1995-05-15 1998-08-25 The Boeing Company System for backdrive of flight deck controls during autopilot operation
US6230642B1 (en) * 1999-08-19 2001-05-15 The Talaria Company, Llc Autopilot-based steering and maneuvering system for boats
JP2005008059A (ja) * 2003-06-19 2005-01-13 Fuji Heavy Ind Ltd 自動操縦装置
FR2894935B1 (fr) * 2005-12-20 2008-03-21 Airbus France Sas Procede et dispositif pour regler l'intensite lumineuse des voyants d'un equipement de controle et de commande dans un poste de pilotage d'avion
DE102006006995B4 (de) * 2006-02-15 2008-09-18 Audi Ag Kraftfahrzeug umfassend ein Lenkrad und ein ein- und ausschaltbares Autopilot-System
FR2929246B1 (fr) 2008-03-26 2010-03-05 Airbus France Procede et dispositif pour la detection d'absences de pilotage manuel et automatique d'un aeronef
FR2984267B1 (fr) 2011-12-19 2015-08-28 Airbus Operations Sas Systeme de commande de l'energie d'un vehicule

Also Published As

Publication number Publication date
FR3024126A1 (fr) 2016-01-29
US20160185448A1 (en) 2016-06-30
US9994303B2 (en) 2018-06-12

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