ES8203758A1 - Perfeccionamientos en los aparatos para la deteccion de ave-rias en actuadores de aeronaves - Google Patents

Perfeccionamientos en los aparatos para la deteccion de ave-rias en actuadores de aeronaves

Info

Publication number
ES8203758A1
ES8203758A1 ES504442A ES504442A ES8203758A1 ES 8203758 A1 ES8203758 A1 ES 8203758A1 ES 504442 A ES504442 A ES 504442A ES 504442 A ES504442 A ES 504442A ES 8203758 A1 ES8203758 A1 ES 8203758A1
Authority
ES
Spain
Prior art keywords
actuator
fault detection
actuator fault
aircraft actuator
model
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
Application number
ES504442A
Other languages
English (en)
Other versions
ES504442A0 (es
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of ES504442A0 publication Critical patent/ES504442A0/es
Publication of ES8203758A1 publication Critical patent/ES8203758A1/es
Expired 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)
  • Control Of Position Or Direction (AREA)
  • Feedback Control In General (AREA)
  • Testing And Monitoring For Control Systems (AREA)
  • Safety Devices In Control Systems (AREA)
  • Fluid-Pressure Circuits (AREA)

Abstract

DISPOSITIVO PARA LA DETECCION DE AVERIAS EN ACTUADORES DE AERONAVES. SE CONECTA UN DETECTOR DE POSICION AL ACTUADOR QUE SUMINISTRA UNA SEÑAL DE POSICION DE EQUILIBRIO EN BUELO RECTILINEO INDICATIVA DE LA POSICION DE DICHO ACTUADOR. UNO MEDIOS DE PROCESO DE SEÑAL SUMINISTRAN UNA SEÑAL DE MANDO DE POSICION, DETECTANDOSE UNA SEÑAL DE ERROR DE POSICION A DICHO ACTUADOR COMO LA DIFERENCIA ENTRE LA SEÑAL DE MANDO DE POSICION Y LA SEÑAL DE POSICION DE EQUILIBRIO, Y OBTENIENDOSE SUCESIVAMENTE UNA SEÑAL DE ERROR DE MODELO, UNA SEÑAL DE ERROR DE RUMBO Y, POR ULTIMO, UNA SEÑAL DE INDICACION DE AVERIA EN RESPUESTA A CUANDO LA SEÑAL DE ERROR DE RUMBO SOBREPASA UNA MAGNITUD DE UMBRAL.
ES504442A 1980-08-26 1981-07-30 Perfeccionamientos en los aparatos para la deteccion de ave-rias en actuadores de aeronaves Expired ES8203758A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/181,510 US4355358A (en) 1980-08-26 1980-08-26 Adaptive aircraft actuator fault detection

Publications (2)

Publication Number Publication Date
ES504442A0 ES504442A0 (es) 1982-05-01
ES8203758A1 true ES8203758A1 (es) 1982-05-01

Family

ID=22664575

Family Applications (1)

Application Number Title Priority Date Filing Date
ES504442A Expired ES8203758A1 (es) 1980-08-26 1981-07-30 Perfeccionamientos en los aparatos para la deteccion de ave-rias en actuadores de aeronaves

Country Status (10)

Country Link
US (1) US4355358A (es)
JP (1) JPS5755409A (es)
AU (1) AU541701B2 (es)
CA (1) CA1165876A (es)
CH (1) CH654535B (es)
DE (1) DE3129313A1 (es)
ES (1) ES8203758A1 (es)
FR (1) FR2489545A1 (es)
GB (1) GB2082794B (es)
IT (1) IT1138500B (es)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3214385A1 (de) * 1982-04-20 1983-11-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung fuer die stabilisierung eines eine magnetspule durchfliessenden stroms
US4592055A (en) * 1983-05-02 1986-05-27 United Technologies Corporation Outer-loop monitor for aircraft automatic flight control system
JPS61500190A (ja) * 1983-10-14 1986-01-30 フオ−ド　モ−タ−　カンパニ− パラメ−タを選択して自己補正する制御システム
US4667472A (en) * 1984-12-28 1987-05-26 The Boeing Company Electric integrated actuator with variable gain hydraulic output
US4805126A (en) * 1985-11-26 1989-02-14 Rodems James D Electronic compensation network
US5214596A (en) * 1986-06-14 1993-05-25 Duetsche Forchungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. System for determining the airspeed of helicopters
GB2196445A (en) * 1986-10-17 1988-04-27 John James Sylvester Derry Condition monitoring equipment for power output devices
US5001646A (en) * 1988-12-19 1991-03-19 Mcdonnell Douglas Corporation Automated helicopter flight control system
US5233512A (en) * 1990-06-21 1993-08-03 General Electric Company Method and apparatus for actuator fault detection
US5097744A (en) * 1991-01-14 1992-03-24 General Electric Company Hydraulic control system
DE4311486A1 (de) * 1993-04-07 1994-10-13 Linde Ag Verfahren zur elektrohydraulischen Ansteuerung von verstellbaren hydraulischen Bauteilen und dafür vorgesehene Steuereinrichtung
US5560559A (en) * 1994-06-30 1996-10-01 Alliedsignal, Inc. Actuation system with active compensation for transient loads
US5607123A (en) * 1994-06-30 1997-03-04 Alliedsignal Inc. Actuation system with passive compensation for transient loads
US5850615A (en) * 1995-12-06 1998-12-15 Mcdonnell Douglas Helicopter Co. Rotor blade swashplate-axis rotation and gyroscopic moments componsator
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
JP3091743B1 (ja) 1999-03-30 2000-09-25 株式会社コミュータヘリコプタ先進技術研究所 操縦装置
US6643569B2 (en) 2001-03-30 2003-11-04 The Regents Of The University Of Michigan Method and system for detecting a failure or performance degradation in a dynamic system such as a flight vehicle
US6480130B1 (en) * 2001-06-28 2002-11-12 Honeywell International Inc. Method for improving repeatability and removing hysteresis from electromechanical actuators
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
EP1607811A1 (de) * 2004-06-18 2005-12-21 Siemens Aktiengesellschaft Verfahren zum Betrieb einer Recheneinheit sowie Signal zur Verarbeitung in einer Recheneinheit
US7593793B2 (en) * 2004-07-30 2009-09-22 The Boeing Company Adaptive control in the presence of input constraints
DE102005059369B4 (de) * 2005-12-13 2012-06-14 Airbus Operations Gmbh Verfahren und Einrichtung zur automatischen Entlastung eines Hochauftriebsflächensystems, insbesondere eines Landeklappensystems, eines Flugzeugs
DE102006011807A1 (de) * 2006-03-15 2007-09-20 Zf Friedrichshafen Ag Verfahren zur Fehlererkennung an einem Aktuator
US7369932B2 (en) * 2006-05-04 2008-05-06 Honeywell International, Inc. System and method for turbine engine fault detection using discrete event system modeling
US7970583B2 (en) * 2007-12-28 2011-06-28 United Technologies Corporation Degraded actuator detection
FR2936067B1 (fr) * 2008-09-18 2012-04-27 Airbus France Procede et dispositif de detection de pannes oscillatoires dans une chaine d'asservissement en position d'une gouverne d'aeronef
JP5437687B2 (ja) * 2009-04-14 2014-03-12 ナブテスコ株式会社 アクチュエータ監視回路、制御装置、およびアクチュエータユニット
US8310193B2 (en) * 2010-01-12 2012-11-13 Hamilton Sundstrand Corporation Minimum temperature control for electromechanical actuator
US8965538B2 (en) * 2010-05-19 2015-02-24 The Boeing Company Methods and apparatus for state limiting in a control system
KR20130116182A (ko) 2012-04-12 2013-10-23 (주)아모레퍼시픽 개선된 사용감을 가지는 발포 폼
JP6178587B2 (ja) * 2013-02-28 2017-08-09 三菱航空機株式会社 航空機のアクチュエータ装置、及び、航空機
US9352831B2 (en) 2013-05-08 2016-05-31 Bell Helicopter Textron Inc. Variable lower limit collective governor to improve recovery
US20180022449A1 (en) * 2016-07-25 2018-01-25 Sikorsky Aircraft Corporation Rotor swashplate actuator position synchronization
US11796990B2 (en) * 2021-08-24 2023-10-24 Woodward, Inc. Model based monitoring of faults in electro-hydraulic valves
CN114545907B (zh) * 2022-03-15 2023-12-19 中南大学 一种基于滤波器的飞行控制系统的故障检测方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5413883A (en) * 1977-07-04 1979-02-01 Hitachi Ltd Abnormalness detector of automatic controller
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
US4249238A (en) * 1978-05-24 1981-02-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus for sensor failure detection and correction in a gas turbine engine control system
US4206891A (en) * 1978-10-26 1980-06-10 United Technologies Corporation Helicopter pedal feel force proportional to side slip
FR2442484A1 (fr) * 1978-11-22 1980-06-20 Materiel Telephonique Dispositif electronique de surveillance de fonctionnement de servoverin hydraulique

Also Published As

Publication number Publication date
ES504442A0 (es) 1982-05-01
GB2082794A (en) 1982-03-10
FR2489545A1 (fr) 1982-03-05
JPS5755409A (en) 1982-04-02
CH654535B (es) 1986-02-28
FR2489545B1 (es) 1984-06-22
US4355358A (en) 1982-10-19
DE3129313A1 (de) 1982-05-06
CA1165876A (en) 1984-04-17
GB2082794B (en) 1984-07-11
IT1138500B (it) 1986-09-17
DE3129313C2 (es) 1990-01-04
AU7347081A (en) 1982-03-04
AU541701B2 (en) 1985-01-17
IT8123634A0 (it) 1981-08-25

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19990503