DE69605478D1 - Überwachungssysteme zur Fehlerdetektion in fly-by-wire Flugsteuerungssystemen - Google Patents

Überwachungssysteme zur Fehlerdetektion in fly-by-wire Flugsteuerungssystemen

Info

Publication number
DE69605478D1
DE69605478D1 DE69605478T DE69605478T DE69605478D1 DE 69605478 D1 DE69605478 D1 DE 69605478D1 DE 69605478 T DE69605478 T DE 69605478T DE 69605478 T DE69605478 T DE 69605478T DE 69605478 D1 DE69605478 D1 DE 69605478D1
Authority
DE
Germany
Prior art keywords
fly
error detection
systems
flight control
wire flight
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 - Lifetime
Application number
DE69605478T
Other languages
English (en)
Other versions
DE69605478T2 (de
Inventor
Alan B Hickman
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of DE69605478D1 publication Critical patent/DE69605478D1/de
Publication of DE69605478T2 publication Critical patent/DE69605478T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • G05B23/0224—Process history based detection method, e.g. whereby history implies the availability of large amounts of data
    • G05B23/0227—Qualitative history assessment, whereby the type of data acted upon, e.g. waveforms, images or patterns, is not relevant, e.g. rule based assessment; if-then decisions
    • G05B23/0237—Qualitative history assessment, whereby the type of data acted upon, e.g. waveforms, images or patterns, is not relevant, e.g. rule based assessment; if-then decisions based on parallel systems, e.g. comparing signals produced at the same time by same type systems and detect faulty ones by noticing differences among their responses
    • 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
    • G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
DE69605478T 1995-05-15 1996-05-15 Überwachungssysteme zur Fehlerdetektion in fly-by-wire Flugsteuerungssystemen Expired - Lifetime DE69605478T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/441,377 US5881971A (en) 1995-05-15 1995-05-15 Monitoring systems for detecting failures in fly-by-wire aircraft flight control systems

Publications (2)

Publication Number Publication Date
DE69605478D1 true DE69605478D1 (de) 2000-01-13
DE69605478T2 DE69605478T2 (de) 2000-04-06

Family

ID=23752640

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69605478T Expired - Lifetime DE69605478T2 (de) 1995-05-15 1996-05-15 Überwachungssysteme zur Fehlerdetektion in fly-by-wire Flugsteuerungssystemen

Country Status (4)

Country Link
US (1) US5881971A (de)
EP (1) EP0743583B1 (de)
JP (1) JP3847373B2 (de)
DE (1) DE69605478T2 (de)

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US6578425B2 (en) * 2001-05-29 2003-06-17 Honeywell Inc. Apparatus and method for verifying the dynamic stiffness capability of hydraulic servo actuators
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US6622972B2 (en) 2001-10-31 2003-09-23 The Boeing Company Method and system for in-flight fault monitoring of flight control actuators
US6813527B2 (en) * 2002-11-20 2004-11-02 Honeywell International Inc. High integrity control system architecture using digital computing platforms with rapid recovery
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FR2855922B1 (fr) * 2003-06-06 2005-08-19 Thales Sa Procede et dispositif de traitement des informations provenant d'equipements primaires de vol repondants
DE10326557A1 (de) * 2003-06-12 2005-01-05 Robert Bosch Gmbh Fehlerdiagnoseverfahren und -vorrichtung
EP1730066B1 (de) * 2004-03-16 2010-10-20 Otis Elevator Company Erfassung von verschleiss und versagen eines aufzuglasttragglieds
US8311697B2 (en) * 2004-07-27 2012-11-13 Honeywell International Inc. Impact assessment system and method for determining emergent criticality
US7243042B2 (en) 2004-11-30 2007-07-10 Siemens Power Generation, Inc. Engine component life monitoring system and method for determining remaining useful component life
DE102005018123B4 (de) * 2005-04-20 2016-10-20 Hottinger Baldwin Messtechnik Gmbh Verfahren zur Bewertung von Messwerten zur Erkennung einer Materialermüdung
WO2007084529A2 (en) * 2006-01-17 2007-07-26 Gulfstream Aerospace Corporation System and method for an integrated backup control system
BRPI0706613A2 (pt) * 2006-01-17 2011-04-05 Gulfstream Aerospace Corp aparelho e método para controle de backup em um sistema de controle de vÈo distribuìdo
US8090485B2 (en) * 2007-11-27 2012-01-03 Embraer S.A. Low-frequency flight control system oscillatory faults prevention via horizontal and vertical tail load monitors
US8489255B2 (en) * 2008-03-17 2013-07-16 Airbus Operations Gmbh Method and device for compensation of mechanical stresses in an aircraft structure
GB2460024B (en) * 2008-05-12 2013-10-16 Rolls Royce Plc Developments in or relating to system prognostics
US8024079B2 (en) * 2008-05-20 2011-09-20 The Boeing Company Wing-body load alleviation for aircraft
FR2932584B1 (fr) * 2008-06-17 2010-11-12 Messier Bugatti Calculateur pour aeronef, capable de gerer plusieurs fonctions
US8342445B2 (en) * 2008-09-26 2013-01-01 The Boeing Company Horizontal tail load alleviation system
US8955365B2 (en) * 2008-12-23 2015-02-17 Embraer S.A. Performance monitoring and prognostics for aircraft pneumatic control valves
FR2946023B1 (fr) * 2009-06-02 2014-11-28 Airbus France Procede et dispositif de traitement de pannes
EP2296064B1 (de) * 2009-09-10 2019-04-24 Sikorsky Aircraft Corporation Leben verbesserndes Flugsteuerungssystem
FR2972712B1 (fr) * 2011-03-16 2014-09-05 Airbus Operations Sas Surveillance d'un actionneur de commande de vol d'un aeronef
US8855943B1 (en) 2011-10-31 2014-10-07 The Boeing Company Fatigue monitoring system and methods
US20130126680A1 (en) * 2011-11-17 2013-05-23 Honeywell International Inc. Unmanned air vehicle fault tolerant flight control system and method
WO2014168673A2 (en) 2013-01-28 2014-10-16 Gulfstream Aerospace Corporation Adaptive oscillatory fault monitoring
US9132911B2 (en) 2013-02-28 2015-09-15 Sikorsky Aircraft Corporation Damage adaptive control
CA3045247A1 (en) 2016-11-30 2018-06-07 Bombardier Inc. Aircraft control system with residual error containment
FR3064979B1 (fr) * 2017-04-07 2019-04-05 Airbus Operations (S.A.S.) Systeme de commande de vol d'un aeronef
WO2019054997A1 (en) 2017-09-13 2019-03-21 Sikorsky Aircraft Corporation CONTROL OF AN AIRCRAFT BASED ON DETECTION AND MITIGATION OF FATIGUE CONDITIONS AND CONDITIONS OF AIRCRAFT DAMAGE
EP3531262A1 (de) * 2018-02-27 2019-08-28 Gulfstream Aerospace Corporation Avioniksysteme mit ereignisabhängiger synoptik
US20190337634A1 (en) * 2018-05-01 2019-11-07 Sikorsky Aircraft Corporation Controlling an Aircraft Based on Detecting Control Element Damage
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US10974851B2 (en) 2018-11-09 2021-04-13 Textron Innovations Inc. System and method for maintaining and configuring rotorcraft
US11748183B2 (en) * 2020-10-11 2023-09-05 Textron Innovations Inc. Reasonableness monitor
FR3127047B1 (fr) * 2021-09-15 2023-09-22 Airbus Operations Sas Système et procédé d’estimation automatique d’une vitesse d’un aéronef lors d’un vol de l’aéronef.
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

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Also Published As

Publication number Publication date
DE69605478T2 (de) 2000-04-06
JP3847373B2 (ja) 2006-11-22
US5881971A (en) 1999-03-16
EP0743583A3 (de) 1996-12-11
EP0743583B1 (de) 1999-12-08
EP0743583A2 (de) 1996-11-20
JPH08310493A (ja) 1996-11-26

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