FR2966616B1 - Procede, dispositif et programme d'ordinateur d'aide au diagnostic d'un systeme d'un aeronef, utilisant des graphes d'evenements redoutes - Google Patents

Procede, dispositif et programme d'ordinateur d'aide au diagnostic d'un systeme d'un aeronef, utilisant des graphes d'evenements redoutes

Info

Publication number
FR2966616B1
FR2966616B1 FR1004161A FR1004161A FR2966616B1 FR 2966616 B1 FR2966616 B1 FR 2966616B1 FR 1004161 A FR1004161 A FR 1004161A FR 1004161 A FR1004161 A FR 1004161A FR 2966616 B1 FR2966616 B1 FR 2966616B1
Authority
FR
France
Prior art keywords
aiding
graphics
aircraft
diagnosis
computer program
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
FR1004161A
Other languages
English (en)
Other versions
FR2966616A1 (fr
Inventor
Vincent Cheriere
Christophe Abelin
Jeremy Roger
Estrada Laia Vilalta
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
Airbus SAS
Original Assignee
Airbus Operations SAS
Airbus 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, Airbus SAS filed Critical Airbus Operations SAS
Priority to FR1004161A priority Critical patent/FR2966616B1/fr
Priority to US13/276,632 priority patent/US8996340B2/en
Priority to CN201110321643.2A priority patent/CN102455704B/zh
Publication of FR2966616A1 publication Critical patent/FR2966616A1/fr
Application granted granted Critical
Publication of FR2966616B1 publication Critical patent/FR2966616B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/07—Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/0703—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation
    • G06F11/079—Root cause analysis, i.e. error or fault diagnosis
    • 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
    • G05B23/0243—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 model based detection method, e.g. first-principles knowledge model
    • G05B23/0245—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 model based detection method, e.g. first-principles knowledge model based on a qualitative model, e.g. rule based; if-then decisions
    • G05B23/0248—Causal models, e.g. fault tree; digraphs; qualitative physics
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/07—Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/0703—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation
    • G06F11/0706—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment
    • G06F11/0736—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment in functional embedded systems, i.e. in a data processing system designed as a combination of hardware and software dedicated to performing a certain function
    • G06F11/0739—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment in functional embedded systems, i.e. in a data processing system designed as a combination of hardware and software dedicated to performing a certain function in a data processing system embedded in automotive or aircraft systems
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/07—Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/0703—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation
    • G06F11/0706—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment
    • G06F11/0748—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment in a remote unit communicating with a single-box computer node experiencing an error/fault

Landscapes

  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Quality & Reliability (AREA)
  • Health & Medical Sciences (AREA)
  • Biomedical Technology (AREA)
  • Computer Hardware Design (AREA)
  • Automation & Control Theory (AREA)
  • Testing And Monitoring For Control Systems (AREA)
FR1004161A 2010-10-22 2010-10-22 Procede, dispositif et programme d'ordinateur d'aide au diagnostic d'un systeme d'un aeronef, utilisant des graphes d'evenements redoutes Active FR2966616B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1004161A FR2966616B1 (fr) 2010-10-22 2010-10-22 Procede, dispositif et programme d'ordinateur d'aide au diagnostic d'un systeme d'un aeronef, utilisant des graphes d'evenements redoutes
US13/276,632 US8996340B2 (en) 2010-10-22 2011-10-19 Method, devices and computer program for assisting in the diagnostic of an aircraft system, using failure condition graphs
CN201110321643.2A CN102455704B (zh) 2010-10-22 2011-10-21 使用可疑事件图进行航空器***诊断辅助的方法、装置

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1004161A FR2966616B1 (fr) 2010-10-22 2010-10-22 Procede, dispositif et programme d'ordinateur d'aide au diagnostic d'un systeme d'un aeronef, utilisant des graphes d'evenements redoutes

Publications (2)

Publication Number Publication Date
FR2966616A1 FR2966616A1 (fr) 2012-04-27
FR2966616B1 true FR2966616B1 (fr) 2012-12-14

Family

ID=43508560

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1004161A Active FR2966616B1 (fr) 2010-10-22 2010-10-22 Procede, dispositif et programme d'ordinateur d'aide au diagnostic d'un systeme d'un aeronef, utilisant des graphes d'evenements redoutes

Country Status (3)

Country Link
US (1) US8996340B2 (fr)
CN (1) CN102455704B (fr)
FR (1) FR2966616B1 (fr)

Families Citing this family (22)

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US20130066924A1 (en) * 2008-12-23 2013-03-14 Honeywell International Inc. Method and apparatus for utilizing matlab functionality in java-enabled environment
DE102011079034A1 (de) 2011-07-12 2013-01-17 Siemens Aktiengesellschaft Ansteuerung eines technischen Systems
US8798817B2 (en) * 2012-01-31 2014-08-05 Gulfstream Aerospace Corporation Methods and systems for requesting and retrieving aircraft data during flight of an aircraft
US20130197739A1 (en) * 2012-01-31 2013-08-01 Gulfstream Aerospace Corporation Methods and systems for aircraft health and trend monitoring
FR2989500B1 (fr) * 2012-04-12 2014-05-23 Airbus Operations Sas Procede, dispositifs et programme d'ordinateur d'aide a l'analyse de la tolerance aux pannes d'un systeme d'un aeronef, utilisant des graphes d'evenements redoutes
US10539955B2 (en) * 2012-06-15 2020-01-21 The Boeing Company Failure analysis validation and visualization
GB2513133B (en) 2013-04-16 2015-07-08 Ge Aviat Systems Ltd Methods for predicting a speed brake system fault
GB2513132B (en) * 2013-04-16 2015-05-27 Ge Aviat Systems Ltd Method for predicting a bleed air system fault
FR3009396B1 (fr) * 2013-07-31 2017-03-17 Airbus Operations Sas Procede et programme d'ordinateur d'aide a la maintenance d'equipements d'un aeronef
FR3011105B1 (fr) 2013-09-20 2017-01-27 Airbus Operations Sas Procede d'identification d'un equipement defaillant dans un aeronef.
US20150149024A1 (en) * 2013-11-22 2015-05-28 Sikorsky Aircraft Corporation Latency tolerant fault isolation
FR3018933A1 (fr) * 2014-03-20 2015-09-25 Airbus Procede de determination de l'etat d'un equipement d'aeronef.
CN105281945B (zh) * 2014-09-19 2020-04-07 中国人民解放军第二炮兵工程大学 基于数据流的确定性网络完整性故障检测方法
US9547944B2 (en) 2015-06-10 2017-01-17 Honeywell International Inc. Health monitoring system for diagnosing and reporting anomalies
JP2019515403A (ja) * 2016-04-11 2019-06-06 ケーピーアイティ テクノロジーズ リミテッド 診断のためのグラフデータベースおよびシステム健康モニタリング
US10599421B2 (en) 2017-07-14 2020-03-24 Calamp Corp. Systems and methods for failsafe firmware upgrades
FR3072647B1 (fr) * 2017-10-24 2019-11-15 Dassault Aviation Systeme de controle d'une trajectoire laterale d'un aeronef incluant un palonnier
SE543122C2 (sv) * 2019-02-05 2020-10-13 Brokk Ab Förfarande, anordning och användargränssnitt som beskriver ett operativt drifttillstånd hos en demoleringsrobot
US11615656B2 (en) 2019-12-20 2023-03-28 Pratt & Whitney Canada Corp. Method and system for diagnosing an engine or an aircraft
CN111736568A (zh) * 2020-05-20 2020-10-02 天津市天锻压力机有限公司 一种实时数据库的故障快速诊断方法及***
CN113268591B (zh) * 2021-04-17 2022-11-01 中国人民解放军战略支援部队信息工程大学 基于事理图谱的空中目标意图判证方法及***
CN114154586B (zh) * 2021-12-09 2022-08-26 中国民用航空飞行学院 一种航空器***定量相似性分析方法、装置及介质

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6223143B1 (en) * 1998-08-31 2001-04-24 The United States Government As Represented By The Administrator Of The National Aeronautics And Space Administration Quantitative risk assessment system (QRAS)
US6820044B2 (en) 2001-10-09 2004-11-16 University Of Maryland Method and apparatus for a common-cause failure module for probabilistic risk assessment tools
US20050065753A1 (en) * 2003-09-24 2005-03-24 International Business Machines Corporation Apparatus and method for monitoring system health based on fuzzy metric data ranges and fuzzy rules
US20070028220A1 (en) * 2004-10-15 2007-02-01 Xerox Corporation Fault detection and root cause identification in complex systems
US7230527B2 (en) * 2004-11-10 2007-06-12 The Boeing Company System, method, and computer program product for fault prediction in vehicle monitoring and reporting system
US7249003B2 (en) * 2005-02-11 2007-07-24 California Institute Of Technology System for solving diagnosis and hitting set problems
FR2891379B1 (fr) * 2005-09-23 2007-11-30 Thales Sa Procede et systeme de diagnostic des pannes pour aerodynes
FR2905763B1 (fr) * 2006-09-11 2008-12-12 Eurocopter France Procede et systeme de diagnostic d'un aeronef a partir de mesures effectuees sur l'aeronef.
CN101063643B (zh) * 2007-02-02 2011-06-29 北京航空航天大学 飞机故障智能诊断方法及***
US8437904B2 (en) * 2007-06-12 2013-05-07 The Boeing Company Systems and methods for health monitoring of complex systems
US8467913B2 (en) * 2007-10-31 2013-06-18 Airbus Operations Gmbh Method and arrangement for providing a fault diagnosis for at least one system
FR2927435B1 (fr) 2008-02-08 2010-02-12 Airbus France Procede et dispositif ameliores pour les operations de diagnostic et de maintenance d'aeronefs
FR2935186B1 (fr) * 2008-08-20 2010-09-17 Airbus France Procede et dispositif d'aide au diagnostic et a la decision d'exploitation d'un aeronef
FR2949161B1 (fr) * 2009-08-14 2011-09-09 Thales Sa Dispositif pour le diagnostic de systeme
CN102416821A (zh) * 2011-07-27 2012-04-18 中国国际航空股份有限公司 飞机***数据处理方法

Also Published As

Publication number Publication date
CN102455704B (zh) 2016-08-03
US20120101793A1 (en) 2012-04-26
CN102455704A (zh) 2012-05-16
FR2966616A1 (fr) 2012-04-27
US8996340B2 (en) 2015-03-31

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