FR2982239B1 - Procede et dispositif de detection du blocage d'une gouverne d'aeronef. - Google Patents

Procede et dispositif de detection du blocage d'une gouverne d'aeronef.

Info

Publication number
FR2982239B1
FR2982239B1 FR1160156A FR1160156A FR2982239B1 FR 2982239 B1 FR2982239 B1 FR 2982239B1 FR 1160156 A FR1160156 A FR 1160156A FR 1160156 A FR1160156 A FR 1160156A FR 2982239 B1 FR2982239 B1 FR 2982239B1
Authority
FR
France
Prior art keywords
blocking
detecting
government
aircraft
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.)
Active
Application number
FR1160156A
Other languages
English (en)
Other versions
FR2982239A1 (fr
Inventor
Philippe Goupil
Remy Dayre
Berre Herve Le
Anca Gheorghe
Ali Zolghadri
Jerome Cieslak
David Henry
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
Centre National de la Recherche Scientifique CNRS
Universite des Sciences et Tech (Bordeaux 1)
Original Assignee
Airbus Operations SAS
Centre National de la Recherche Scientifique CNRS
Universite des Sciences et Tech (Bordeaux 1)
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, Centre National de la Recherche Scientifique CNRS, Universite des Sciences et Tech (Bordeaux 1) filed Critical Airbus Operations SAS
Priority to FR1160156A priority Critical patent/FR2982239B1/fr
Priority to US13/671,964 priority patent/US8755956B2/en
Publication of FR2982239A1 publication Critical patent/FR2982239A1/fr
Application granted granted Critical
Publication of FR2982239B1 publication Critical patent/FR2982239B1/fr
Active 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
    • G05D3/00—Control of position or direction
    • G05D3/12—Control of position or direction using feedback
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B23/00—Testing or monitoring of control systems or parts thereof
    • G05B23/02—Electric testing or monitoring
    • G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
    • G05B23/0218—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterised by the fault detection method dealing with either existing or incipient faults
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M17/00—Testing of vehicles
    • 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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot

Abstract

- Le dispositif de détection (1) comporte des moyens (20) pour déterminer une erreur d'asservissement correspondant à l'écart entre un premier ordre de commande et une position de gouverne, des moyens (22) pour calculer la différence entre cette erreur d'asservissement et un second ordre de commande de manière à former un signal de comparaison, et des moyens (27) pour détecter un blocage de la gouverne, si ce signal de comparaison est supérieur à une valeur de seuil.
FR1160156A 2011-11-08 2011-11-08 Procede et dispositif de detection du blocage d'une gouverne d'aeronef. Active FR2982239B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1160156A FR2982239B1 (fr) 2011-11-08 2011-11-08 Procede et dispositif de detection du blocage d'une gouverne d'aeronef.
US13/671,964 US8755956B2 (en) 2011-11-08 2012-11-08 Method and device for detecting the jamming of an aircraft control surface

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1160156A FR2982239B1 (fr) 2011-11-08 2011-11-08 Procede et dispositif de detection du blocage d'une gouverne d'aeronef.

Publications (2)

Publication Number Publication Date
FR2982239A1 FR2982239A1 (fr) 2013-05-10
FR2982239B1 true FR2982239B1 (fr) 2014-05-09

Family

ID=45375448

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1160156A Active FR2982239B1 (fr) 2011-11-08 2011-11-08 Procede et dispositif de detection du blocage d'une gouverne d'aeronef.

Country Status (2)

Country Link
US (1) US8755956B2 (fr)
FR (1) FR2982239B1 (fr)

Families Citing this family (12)

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US10065728B2 (en) * 2011-06-30 2018-09-04 Parker-Hannifin Corporation Horizontal stabilizer trim actuator failure detection system and method using position sensors
US20140343765A1 (en) 2012-12-28 2014-11-20 Sean Patrick Suiter Flight Assistant with Automatic Configuration and Landing Site Selection
US11657721B1 (en) 2013-08-26 2023-05-23 Otto Aero Company Aircraft with flight assistant
US9284043B2 (en) * 2013-11-21 2016-03-15 Aai Corporation Evaluating aileron deflection while an unmanned aerial vehicle is in flight
US9193455B2 (en) * 2014-02-19 2015-11-24 Sikorsky Aircraft Corporation Fly by wire servos with internal loop closure
FR3020036B1 (fr) * 2014-04-16 2017-11-24 Airbus Operations Sas Systeme d'actionneur pour gouverne d'aeronef.
DE102014219848A1 (de) * 2014-09-30 2016-03-31 Airbus Operations Gmbh Überwachungsvorrichtung für Differentialtransformator-Sensoren in einem Flugzeug und Verfahren
WO2016199016A1 (fr) * 2015-06-12 2016-12-15 Bombardier Inc. Procédés, dispositifs et systèmes d'indication pour surfaces de commande de vol à portance élevée d'aéronef
US10604236B2 (en) 2016-06-01 2020-03-31 Regents Of The University Of Minnesota Fault-tolerant aircraft flight control using a subset of aerodynamic control surfaces
US10933978B2 (en) 2017-01-10 2021-03-02 Parker-Hannifin Corporation Moving end electronic detection of secondary load path engagement of aircraft flight control actuator
US10479484B2 (en) * 2017-06-14 2019-11-19 The Boeing Company Methods and apparatus for controlling aircraft flight control surfaces
US10843792B2 (en) * 2018-02-01 2020-11-24 Hamilton Sundstrand Corporation Autonomous reconfiguration of a multi-redundant actuator control system

Family Cites Families (16)

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Publication number Priority date Publication date Assignee Title
FR2344063A1 (fr) * 1976-03-10 1977-10-07 Smiths Industries Ltd Circuit numerique de commande a deux voies au moins
US4148452A (en) * 1977-12-08 1979-04-10 The United States Of America As Represented By The Administrator, National Aeronautics And Space Administration Filtering technique based on high-frequency plant modeling for high-gain control
US4472780A (en) * 1981-09-28 1984-09-18 The Boeing Company Fly-by-wire lateral control system
US4649484A (en) * 1983-08-01 1987-03-10 The Boeing Company Avionic control system
US5274554A (en) * 1991-02-01 1993-12-28 The Boeing Company Multiple-voting fault detection system for flight critical actuation control systems
US5615119A (en) * 1995-06-07 1997-03-25 Aurora Flight Sciences Corporation Fault tolerant automatic control system utilizing analytic redundancy
US6085127A (en) * 1997-03-18 2000-07-04 Aurora Flight Sciences Corporation Fault tolerant automatic control system utilizing analytic redundancy
US7451021B2 (en) * 2003-05-06 2008-11-11 Edward Wilson Model-based fault detection and isolation for intermittently active faults with application to motion-based thruster fault detection and isolation for spacecraft
US7209809B2 (en) * 2003-10-15 2007-04-24 The Boeing Company Method and apparatus for obtaining high integrity and availability in multi-channel systems
US7098619B2 (en) * 2004-01-28 2006-08-29 Stridsberg Innovation Ab Actuator and movement linkage system
FR2893911B1 (fr) * 2005-11-28 2007-12-21 Airbus France Sas Procede et dispositif de detection de pannes oscillatoires dans une chaine d'asservissement en position d'une gouverne d'aeronef
US8725321B2 (en) * 2006-05-17 2014-05-13 Textron Innovations Inc. Flight control system
US7567862B2 (en) * 2007-08-14 2009-07-28 The Boeing Company Actuation response oscillation detection monitor
US8080966B2 (en) * 2008-07-03 2011-12-20 Honeywell International Inc. Motor control architecture for simultaneously controlling multiple motors
DE102008052754A1 (de) * 2008-10-22 2010-05-06 Airbus Deutschland Gmbh Verstellvorrichtung zur Ankopplung an eine Verstellklappe eines Flugzeugs, fehlertolerantes Stellsystem und Verfahren zur Rekonfiguration eines Stellsystems
DE102009061036B4 (de) * 2009-04-28 2016-03-31 Airbus Operations Gmbh Vorrichtung und Verfahren zur Residuengenerierung zur Erkennung von fehlerhaften Transienten, Drift oder Oszillationen im Systemverhalten eines Systems eines Flugzeugs, und Flugzeug

Also Published As

Publication number Publication date
FR2982239A1 (fr) 2013-05-10
US20130116863A1 (en) 2013-05-09
US8755956B2 (en) 2014-06-17

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