DE602007001839D1 - Einstellverfahren für die Fehlererkennung bei Flugzeugen - Google Patents

Einstellverfahren für die Fehlererkennung bei Flugzeugen

Info

Publication number
DE602007001839D1
DE602007001839D1 DE602007001839T DE602007001839T DE602007001839D1 DE 602007001839 D1 DE602007001839 D1 DE 602007001839D1 DE 602007001839 T DE602007001839 T DE 602007001839T DE 602007001839 T DE602007001839 T DE 602007001839T DE 602007001839 D1 DE602007001839 D1 DE 602007001839D1
Authority
DE
Germany
Prior art keywords
fault detection
setting procedure
aircraft fault
aircraft
procedure
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
DE602007001839T
Other languages
English (en)
Inventor
Subhabrata Ganguli
George Papageorgiou
Sonja Glavaski-Radovanovic
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.)
Honeywell Inc
Original Assignee
Honeywell Inc
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 Honeywell Inc filed Critical Honeywell Inc
Publication of DE602007001839D1 publication Critical patent/DE602007001839D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0047—Navigation or guidance aids for a single aircraft
    • G08G5/0052—Navigation or guidance aids for a single aircraft for cruising
    • 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
    • G05B23/0254—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 quantitative model, e.g. mathematical relationships between inputs and outputs; functions: observer, Kalman filter, residual calculation, Neural Networks
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G08G5/0021—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Artificial Intelligence (AREA)
  • Evolutionary Computation (AREA)
  • Mathematical Physics (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)
DE602007001839T 2006-08-04 2007-05-04 Einstellverfahren für die Fehlererkennung bei Flugzeugen Active DE602007001839D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/462,481 US8209083B2 (en) 2006-08-04 2006-08-04 Tunable architecture for aircraft fault detection

Publications (1)

Publication Number Publication Date
DE602007001839D1 true DE602007001839D1 (de) 2009-09-17

Family

ID=38278938

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007001839T Active DE602007001839D1 (de) 2006-08-04 2007-05-04 Einstellverfahren für die Fehlererkennung bei Flugzeugen

Country Status (3)

Country Link
US (1) US8209083B2 (de)
EP (1) EP1884852B1 (de)
DE (1) DE602007001839D1 (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
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US8255100B2 (en) * 2008-02-27 2012-08-28 The Boeing Company Data-driven anomaly detection to anticipate flight deck effects
US8352099B1 (en) * 2009-07-09 2013-01-08 The Boeing Company Varying engine thrust for directional control of an aircraft experiencing engine thrust asymmetry
FR2953954B1 (fr) * 2009-12-11 2012-10-12 Thales Sa Dispositif d'elaboration des alertes d'un systeme d'aeronef
FR2986065B1 (fr) * 2012-01-23 2015-04-17 Airbus Operations Sas Procede et dispositif d'affichage d'informations d'assiette sur un avion lors d'un decollage.
CN102968059B (zh) * 2012-08-10 2016-07-13 中国商用飞机有限责任公司 飞机起落架模拟器
CN103970024A (zh) * 2013-01-29 2014-08-06 中国航空工业集团公司西安飞机设计研究所 一种大型飞机液压系统实时仿真系统
FR3002048B1 (fr) * 2013-02-14 2016-07-01 Commissariat Energie Atomique Procede de detection amelioree de collision d'un robot avec son environnement, systeme et produit programme d'ordinateur mettant en œuvre le procede
US9825641B1 (en) 2014-09-12 2017-11-21 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Reconfigurable sensor monitoring system
CN105488281B (zh) * 2015-12-01 2019-01-15 北京航空航天大学 一种基于飞行参数监控的飞机结构载荷识别方法
CA3026051A1 (en) * 2016-05-31 2017-12-07 Bombardier Inc. Displaying performance limitations in aircraft display
US10147244B2 (en) 2016-06-10 2018-12-04 Simmonds Precision Products, Inc. Fault source parameter identification
CN108454879B (zh) 2016-12-12 2022-08-02 中国国际航空股份有限公司 飞机故障处理系统和方法及计算机设备
US10592636B2 (en) * 2017-03-17 2020-03-17 General Electric Company Methods and systems for flight data based parameter tuning and deployment
US10657736B2 (en) * 2017-09-25 2020-05-19 The Boeing Company System and method for aircraft fault detection
US10650614B2 (en) * 2017-09-29 2020-05-12 The Boeing Company Aircraft maintenance event prediction using higher-level and lower-level system information
US10787278B2 (en) 2017-09-29 2020-09-29 The Boeing Company Aircraft maintenance message prediction
US10719772B2 (en) * 2017-10-27 2020-07-21 The Boeing Company Unsupervised multivariate relational fault detection system for a vehicle and method therefor
US10672204B2 (en) * 2017-11-15 2020-06-02 The Boeing Company Real time streaming analytics for flight data processing
CN109522944B (zh) * 2018-10-30 2022-12-13 中国运载火箭技术研究院 一种空间飞行器故障多维度快速分类方法
FR3103283B1 (fr) * 2019-11-20 2022-07-29 Thales Sa Dispositif electronique et procede d'estimation de position(s) d'element(s) de trafic aerien, systeme d'affichage et programme d'ordinateur associes
US11815608B2 (en) 2020-07-28 2023-11-14 Honeywell International Inc. Vector air data dynamic constraining and self-checking systems and methods
CN112407307A (zh) * 2020-11-20 2021-02-26 中国直升机设计研究所 一种直升机飞控系统综合显示方法
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 (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4022954A1 (de) 1990-07-19 1992-01-23 Bodenseewerk Geraetetech Fehlerdetektor bei redundant vorgesehenen signalgebern
US5719566A (en) 1996-06-28 1998-02-17 Sundstrand Corporation Method and apparatus for detecting dormant actuator failure
US6622134B1 (en) * 1999-01-05 2003-09-16 International Business Machines Corporation Method of constructing data classifiers and classifiers constructed according to the method
US6298286B1 (en) 1999-12-17 2001-10-02 Rockwell Collins Method of preventing potentially hazardously misleading attitude data
US6408259B1 (en) 2000-02-01 2002-06-18 General Electric Company Alert generation for trend performance analysis
US6711523B2 (en) * 2001-05-24 2004-03-23 Simmonds Precision Products, Inc. Method and apparatus for determining a condition indicator for use in evaluating the health of a component
US7356187B2 (en) * 2004-04-12 2008-04-08 Clairvoyance Corporation Method and apparatus for adjusting the model threshold of a support vector machine for text classification and filtering

Also Published As

Publication number Publication date
US20100241293A1 (en) 2010-09-23
US8209083B2 (en) 2012-06-26
EP1884852A1 (de) 2008-02-06
EP1884852B1 (de) 2009-08-05

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Legal Events

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