AU2001277586A1 - Method and device for controlling an aircraft manoeuvring components, with electrical standby modules - Google Patents

Method and device for controlling an aircraft manoeuvring components, with electrical standby modules

Info

Publication number
AU2001277586A1
AU2001277586A1 AU2001277586A AU7758601A AU2001277586A1 AU 2001277586 A1 AU2001277586 A1 AU 2001277586A1 AU 2001277586 A AU2001277586 A AU 2001277586A AU 7758601 A AU7758601 A AU 7758601A AU 2001277586 A1 AU2001277586 A1 AU 2001277586A1
Authority
AU
Australia
Prior art keywords
maneuvering
unit
controlling
detection system
failure detection
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.)
Abandoned
Application number
AU2001277586A
Inventor
Jean-Pierre Garcia
Jean-Marc Ortega
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
Publication of AU2001277586A1 publication Critical patent/AU2001277586A1/en
Abandoned 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
    • G05D1/0055—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Safety Devices In Control Systems (AREA)
  • Selective Calling Equipment (AREA)
  • Steering-Linkage Mechanisms And Four-Wheel Steering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Traffic Control Systems (AREA)

Abstract

A device for controlling aircraft maneuvering units includes at least one control unit and a central computing unit. The control unit may be actuated by a pilot for issuing maneuvering commands. The central computing unit is capable of establishing control signals for at least one maneuvering unit from the maneuvering commands. Each central computing unit is being provided with its own failure detection system. The device further includes at least one backup electronic module respectively associated with a maneuvering unit and capable of also establishing control signals for this maneuvering unit from maneuvering commands. The electronic module lacks any failure detection system of its own, but it is connected to a central failure detection system.
AU2001277586A 2000-07-13 2001-07-12 Method and device for controlling an aircraft manoeuvring components, with electrical standby modules Abandoned AU2001277586A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0009196A FR2811780B1 (en) 2000-07-13 2000-07-13 METHOD AND DEVICE FOR CONTROLLING MANEUVERING DEVICES OF AN AIRCRAFT WITH ELECTRIC BACKUP MODULES
FR0009196 2000-07-13
PCT/FR2001/002275 WO2002006908A1 (en) 2000-07-13 2001-07-12 Method and device for controlling an aircraft manoeuvring components, with electrical standby modules

Publications (1)

Publication Number Publication Date
AU2001277586A1 true AU2001277586A1 (en) 2002-01-30

Family

ID=8852468

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001277586A Abandoned AU2001277586A1 (en) 2000-07-13 2001-07-12 Method and device for controlling an aircraft manoeuvring components, with electrical standby modules

Country Status (9)

Country Link
US (1) US6704624B2 (en)
EP (1) EP1307798B8 (en)
AT (1) ATE441142T1 (en)
AU (1) AU2001277586A1 (en)
BR (1) BR0106936B1 (en)
CA (1) CA2384161C (en)
DE (1) DE60139697D1 (en)
FR (1) FR2811780B1 (en)
WO (1) WO2002006908A1 (en)

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US7946528B2 (en) * 2005-04-15 2011-05-24 Urban Aeronautics, Ltd. Flight control system especially suited for VTOL vehicles
US7717368B2 (en) * 2005-06-07 2010-05-18 Urban Aeronautics Ltd. Apparatus for generating horizontal forces in aerial vehicles and related method
US7549605B2 (en) * 2005-06-27 2009-06-23 Honeywell International Inc. Electric flight control surface actuation system for aircraft flaps and slats
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JP2009523657A (en) * 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 System and method for an integrated backup control system
US8020804B2 (en) 2006-03-01 2011-09-20 Urban Aeronautics, Ltd. Ground effect vanes arrangement
US8833692B2 (en) 2006-11-27 2014-09-16 Urban Aeronautics Ltd. Wall effects on VTOL vehicles
WO2008065664A2 (en) * 2006-11-30 2008-06-05 Urban Aeronautics Ltd. Flight control cockpit modes in ducted fan vtol vehicles
FR2912374B1 (en) * 2007-02-08 2009-05-08 Goodrich Actuation Systems Sas DETECTION OF THE RETURN OF EFFORT BY A SECONDARY CHANNEL OF A FLIGHT CONTROL ACTUATOR
FR2913949B1 (en) * 2007-03-23 2009-10-02 Goodrich Actuation Systems Sas IMPROVEMENTS IN THE DETECTION OF THE RETRIEVAL OF EFFORT OF THE SECONDARY PATH OF A FLIGHT CONTROL ACTUATOR.
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DE102008022092A1 (en) * 2008-05-05 2009-11-19 Airbus Deutschland Gmbh Fault-tolerant control system for adjusting the flaps of an aircraft with adjustable kinematics with a fixed axis of rotation
US8342441B2 (en) 2008-09-02 2013-01-01 Urban Aeronautics Ltd. VTOL vehicle with coaxially tilted or tiltable rotors
FR2939528B1 (en) 2008-12-08 2011-02-11 Airbus France DEVICE AND METHOD FOR AUTOMATICALLY GENERATING AN ORDER FOR CONTROLLING AN AIRCRAFT GOVERNMENT
US8504221B2 (en) * 2009-01-16 2013-08-06 The Boeing Company Apparatus and method for controlling a control surface of a vehicle based on a load identified on the control surface
US8451144B2 (en) * 2009-02-04 2013-05-28 Honeywell International Inc. Flaps overspeed advisory system
FR2943036B1 (en) * 2009-03-11 2011-04-15 Airbus France DISTRIBUTED FLIGHT CONTROL SYSTEM IMPLEMENTED ACCORDING TO AN INTEGRATED MODULAR AVIONIC ARCHITECTURE.
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JP5391086B2 (en) * 2010-01-12 2014-01-15 ナブテスコ株式会社 Flight control system
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US8935015B2 (en) 2011-05-09 2015-01-13 Parker-Hannifin Corporation Flight control system with alternate control path
CN105121188B (en) 2013-03-15 2019-03-15 特力飞车股份有限公司 With the combined flight/driving vehicle to take off vertically with fixed-wing cruising ability
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FR3016607B1 (en) * 2014-01-20 2016-01-22 Sagem Defense Securite ACTUATOR FOR CONTROLLING A HORIZONTAL STABILIZATION PLAN OF AN AIRCRAFT
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Also Published As

Publication number Publication date
FR2811780B1 (en) 2002-08-30
US20020116096A1 (en) 2002-08-22
EP1307798A1 (en) 2003-05-07
DE60139697D1 (en) 2009-10-08
ATE441142T1 (en) 2009-09-15
EP1307798B1 (en) 2009-08-26
US6704624B2 (en) 2004-03-09
CA2384161C (en) 2010-10-26
WO2002006908A1 (en) 2002-01-24
BR0106936A (en) 2002-05-14
FR2811780A1 (en) 2002-01-18
CA2384161A1 (en) 2002-01-24
EP1307798B8 (en) 2009-10-07
BR0106936B1 (en) 2013-05-28

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