AU2001274729A1 - System and method for maintenance - Google Patents

System and method for maintenance

Info

Publication number
AU2001274729A1
AU2001274729A1 AU2001274729A AU7472901A AU2001274729A1 AU 2001274729 A1 AU2001274729 A1 AU 2001274729A1 AU 2001274729 A AU2001274729 A AU 2001274729A AU 7472901 A AU7472901 A AU 7472901A AU 2001274729 A1 AU2001274729 A1 AU 2001274729A1
Authority
AU
Australia
Prior art keywords
maintenance
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.)
Abandoned
Application number
AU2001274729A
Inventor
Dag Folkesson
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.)
Saab AB
Original Assignee
Saab AB
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 Saab AB filed Critical Saab AB
Publication of AU2001274729A1 publication Critical patent/AU2001274729A1/en
Abandoned legal-status Critical Current

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
    • G06F11/0706—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
    • 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
    • G06F11/0751—Error or fault detection not based on redundancy
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
    • G06Q10/00—Administration; Management
    • G06Q10/06—Resources, workflows, human or project management; Enterprise or organisation planning; Enterprise or organisation modelling
    • 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
    • G06F11/0751—Error or fault detection not based on redundancy
    • G06F11/0754—Error or fault detection not based on redundancy by exceeding limits
    • G06F11/0757—Error or fault detection not based on redundancy by exceeding limits by exceeding a time limit, i.e. time-out, e.g. watchdogs
    • 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
    • G06F11/0751—Error or fault detection not based on redundancy
    • G06F11/0754—Error or fault detection not based on redundancy by exceeding limits
    • G06F11/076—Error or fault detection not based on redundancy by exceeding limits by exceeding a count or rate limit, e.g. word- or bit count limit
AU2001274729A 2000-06-13 2001-06-07 System and method for maintenance Abandoned AU2001274729A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE0002195 2000-06-13
SE0002195A SE518104C2 (en) 2000-06-13 2000-06-13 Software maintenance system and method
PCT/SE2001/001327 WO2001097038A1 (en) 2000-06-13 2001-06-07 System and method for maintenance

Publications (1)

Publication Number Publication Date
AU2001274729A1 true AU2001274729A1 (en) 2001-12-24

Family

ID=20280063

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001274729A Abandoned AU2001274729A1 (en) 2000-06-13 2001-06-07 System and method for maintenance

Country Status (5)

Country Link
US (1) US7287195B1 (en)
EP (1) EP1297427A1 (en)
AU (1) AU2001274729A1 (en)
SE (1) SE518104C2 (en)
WO (1) WO2001097038A1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2859556B1 (en) * 2003-09-05 2005-11-11 Airbus France METHOD AND DEVICE FOR MAINTENANCE OF A RADIONAVIGATION EQUIPMENT OF AN AIRCRAFT
US7526677B2 (en) * 2005-10-31 2009-04-28 Microsoft Corporation Fragility handling
US9225684B2 (en) 2007-10-29 2015-12-29 Microsoft Technology Licensing, Llc Controlling network access
JP4453764B2 (en) * 2008-02-22 2010-04-21 トヨタ自動車株式会社 Vehicle diagnostic device, vehicle diagnostic system, and diagnostic method
US7921337B2 (en) * 2008-05-30 2011-04-05 Honeywell International Inc. Systems and methods for diagnosing faults in electronic systems
FR2934397A1 (en) * 2008-07-28 2010-01-29 Eurocopter France IMPROVED METHOD FOR ORGANIZING AIRCRAFT MAINTENANCE
DE102014213503A1 (en) * 2014-07-11 2016-01-14 Bayerische Motoren Werke Aktiengesellschaft Method for monitoring software in a road vehicle

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4698785A (en) * 1983-12-02 1987-10-06 Desmond John P Method and apparatus for detecting control system data processing errors
US4644494A (en) * 1984-02-06 1987-02-17 Sundstrand Data Control, Inc. Solid state memory for aircraft flight data recorder systems
EP0218979B1 (en) * 1985-10-03 1991-04-24 Mitsubishi Denki Kabushiki Kaisha Computer program debugging system
US5184312A (en) * 1985-10-13 1993-02-02 The Boeing Company Distributed built-in test equipment system for digital avionics
US4890284A (en) * 1988-02-22 1989-12-26 United Technologies Corporation Backup control system (BUCS)
US4943919A (en) * 1988-10-17 1990-07-24 The Boeing Company Central maintenance computer system and fault data handling method
US5111402A (en) * 1990-01-19 1992-05-05 Boeing Company Integrated aircraft test system
US5218547A (en) * 1991-05-20 1993-06-08 Tebbs Mark C Universal memory loader verifier
CA2072169A1 (en) * 1991-06-24 1992-12-25 Lih-Juan L. Danielson In-band/out-of-band alert delivery system
US6009370A (en) * 1993-07-26 1999-12-28 Hitachi, Ltd. Control unit for vehicle and total control system therefor
DE69414322T2 (en) * 1993-07-26 1999-05-20 Hitachi Ltd Control unit for a vehicle and an entire control system therefor
US5495268A (en) * 1993-10-20 1996-02-27 Sundstrand Corporation Display system for GCU maintenance information
US5809293A (en) * 1994-07-29 1998-09-15 International Business Machines Corporation System and method for program execution tracing within an integrated processor
US5541863A (en) * 1994-09-30 1996-07-30 Rockwell International Virtual integrated software testbed for avionics
JP3304649B2 (en) 1994-11-22 2002-07-22 三菱電機株式会社 Central monitoring device
US5872909A (en) * 1995-01-24 1999-02-16 Wind River Systems, Inc. Logic analyzer for software
US5974568A (en) * 1995-11-17 1999-10-26 Mci Communications Corporation Hierarchical error reporting system
DE19653429C2 (en) 1996-12-20 1998-10-15 Siemens Ag Method for checking the functionality of a computing unit
JPH10275013A (en) * 1997-03-31 1998-10-13 Meidensha Corp Maintenance support system
US6115656A (en) * 1997-06-17 2000-09-05 Mcdonnell Douglas Corporation Fault recording and reporting method
US6234799B1 (en) * 1998-04-06 2001-05-22 American Gnc Corporation Real-time IMU simulator
DE19841260B4 (en) 1998-09-09 2012-06-14 Continental Automotive Gmbh Method for detecting fault conditions and on-board diagnostic system

Also Published As

Publication number Publication date
SE518104C2 (en) 2002-08-27
WO2001097038A1 (en) 2001-12-20
SE0002195D0 (en) 2000-06-13
EP1297427A1 (en) 2003-04-02
US7287195B1 (en) 2007-10-23
SE0002195L (en) 2001-12-14

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