FR2964205B1 - Systeme de commande d'un aeronef - Google Patents

Systeme de commande d'un aeronef

Info

Publication number
FR2964205B1
FR2964205B1 FR1157536A FR1157536A FR2964205B1 FR 2964205 B1 FR2964205 B1 FR 2964205B1 FR 1157536 A FR1157536 A FR 1157536A FR 1157536 A FR1157536 A FR 1157536A FR 2964205 B1 FR2964205 B1 FR 2964205B1
Authority
FR
France
Prior art keywords
aircraft
control system
control
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
FR1157536A
Other languages
English (en)
Other versions
FR2964205A1 (fr
Inventor
Matthias Stiefenhofer
Matthias Ludwig
Michael Rottach
Ralph Neumann
Manfred Schlosser
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.)
Liebherr Aerospace Lindenberg GmbH
Original Assignee
Liebherr Aerospace Lindenberg GmbH
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 Liebherr Aerospace Lindenberg GmbH filed Critical Liebherr Aerospace Lindenberg GmbH
Publication of FR2964205A1 publication Critical patent/FR2964205A1/fr
Application granted granted Critical
Publication of FR2964205B1 publication Critical patent/FR2964205B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • G05D1/0055—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
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F3/00—Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
    • G06F3/01—Input arrangements or combined input and output arrangements for interaction between user and computer
    • G06F3/016—Input arrangements with force or tactile feedback as computer generated output to the user

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Human Computer Interaction (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Feedback Control In General (AREA)
  • Small-Scale Networks (AREA)
  • Traffic Control Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Mechanical Control Devices (AREA)
FR1157536A 2010-08-30 2011-08-25 Systeme de commande d'un aeronef Expired - Fee Related FR2964205B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102010035822A DE102010035822A1 (de) 2010-08-30 2010-08-30 Steuersystem für ein Luftfahrzeug

Publications (2)

Publication Number Publication Date
FR2964205A1 FR2964205A1 (fr) 2012-03-02
FR2964205B1 true FR2964205B1 (fr) 2017-07-14

Family

ID=45565980

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1157536A Expired - Fee Related FR2964205B1 (fr) 2010-08-30 2011-08-25 Systeme de commande d'un aeronef

Country Status (5)

Country Link
US (1) US20120056039A1 (fr)
BR (1) BRPI1107029A2 (fr)
DE (1) DE102010035822A1 (fr)
FR (1) FR2964205B1 (fr)
RU (1) RU2011136025A (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9199722B2 (en) * 2012-10-09 2015-12-01 Robert Dennis Kennedy Electronic flight controls with parallel processed torque and positioning for pilot or astronaut touch feedback
US20160122001A1 (en) * 2014-11-01 2016-05-05 Robert Dennis Kennedy Electronic flight controls with parallel processed torque & positioning for pilot or astronaut touch feedback
US11939085B2 (en) 2021-06-16 2024-03-26 Beta Air, Llc Methods and systems for wrapping simulated intra-aircraft communication to a physical controller area network
WO2023209335A1 (fr) * 2022-04-29 2023-11-02 Bae Systems Plc Unité de commande dans un organe de pilotage actif
EP4269235A1 (fr) * 2022-04-29 2023-11-01 BAE SYSTEMS plc Unité de commande dans un incepteur actif
GB2618154A (en) * 2022-04-29 2023-11-01 Bae Systems Plc A control unit in an active inceptor

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2807902C2 (de) * 1978-02-24 1980-04-30 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Steuereinrichtung mit aktiver Kraft rückführung
US5493497A (en) * 1992-06-03 1996-02-20 The Boeing Company Multiaxis redundant fly-by-wire primary flight control system
US5264768A (en) * 1992-10-06 1993-11-23 Honeywell, Inc. Active hand controller feedback loop
FR2728537A1 (fr) * 1994-12-21 1996-06-28 Eurocopter France Dispositif pour l'actionnement d'un organe commande pour un aeronef, tel que notamment un helicoptere, a commandes de vol electriques
US5797564A (en) * 1995-05-15 1998-08-25 The Boeing Company System for backdrive of flight deck controls during autopilot operation
US20040078121A1 (en) * 2002-10-22 2004-04-22 Cartmell Daniel H. Control system and method with multiple linked inputs
US7285932B2 (en) * 2003-10-28 2007-10-23 United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method and apparatus for loss of control inhibitor systems
US7367530B2 (en) * 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
US20090187292A1 (en) * 2008-01-17 2009-07-23 Mark Andrew Hreha Integrated pitch, roll, and yaw inceptor
JP4691121B2 (ja) * 2008-02-20 2011-06-01 三菱重工業株式会社 操縦システム、操縦桿リンク切り離し方法

Also Published As

Publication number Publication date
DE102010035822A1 (de) 2012-03-01
US20120056039A1 (en) 2012-03-08
RU2011136025A (ru) 2013-03-10
BRPI1107029A2 (pt) 2014-04-29
FR2964205A1 (fr) 2012-03-02

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