FR2715747B1 - Procédé et dispositif pour rechercher des messages de maintenance intempestifs. - Google Patents

Procédé et dispositif pour rechercher des messages de maintenance intempestifs.

Info

Publication number
FR2715747B1
FR2715747B1 FR9401062A FR9401062A FR2715747B1 FR 2715747 B1 FR2715747 B1 FR 2715747B1 FR 9401062 A FR9401062 A FR 9401062A FR 9401062 A FR9401062 A FR 9401062A FR 2715747 B1 FR2715747 B1 FR 2715747B1
Authority
FR
France
Prior art keywords
searching
maintenance messages
untimely maintenance
untimely
messages
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
FR9401062A
Other languages
English (en)
Other versions
FR2715747A1 (fr
Inventor
Christian Callay
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 Group SAS
Original Assignee
Airbus Group 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 Group SAS filed Critical Airbus Group SAS
Priority to FR9401062A priority Critical patent/FR2715747B1/fr
Priority to US08/377,609 priority patent/US5610923A/en
Publication of FR2715747A1 publication Critical patent/FR2715747A1/fr
Application granted granted Critical
Publication of FR2715747B1 publication Critical patent/FR2715747B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • G06F11/0751—Error or fault detection not based on redundancy
    • 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
    • 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
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L1/00—Arrangements for detecting or preventing errors in the information received
    • H04L1/24—Testing correct operation
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/22—Detection or location of defective computer hardware by testing during standby operation or during idle time, e.g. start-up testing
    • G06F11/2294—Detection or location of defective computer hardware by testing during standby operation or during idle time, e.g. start-up testing by remote test
FR9401062A 1994-02-01 1994-02-01 Procédé et dispositif pour rechercher des messages de maintenance intempestifs. Expired - Lifetime FR2715747B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR9401062A FR2715747B1 (fr) 1994-02-01 1994-02-01 Procédé et dispositif pour rechercher des messages de maintenance intempestifs.
US08/377,609 US5610923A (en) 1994-02-01 1995-01-25 Method and device for finding spurious maintenance messages

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9401062A FR2715747B1 (fr) 1994-02-01 1994-02-01 Procédé et dispositif pour rechercher des messages de maintenance intempestifs.

Publications (2)

Publication Number Publication Date
FR2715747A1 FR2715747A1 (fr) 1995-08-04
FR2715747B1 true FR2715747B1 (fr) 1996-03-01

Family

ID=9459606

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9401062A Expired - Lifetime FR2715747B1 (fr) 1994-02-01 1994-02-01 Procédé et dispositif pour rechercher des messages de maintenance intempestifs.

Country Status (2)

Country Link
US (1) US5610923A (fr)
FR (1) FR2715747B1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2742897B1 (fr) * 1995-12-22 1998-02-20 Aerospatiale Dispositif de surveillance d'un systeme complexe, notamment d'un aeronef
FR2778766B1 (fr) * 1998-05-18 2001-09-07 Eurocopter France Procede et dispositif d'aide a la maintenance d'un aeronef, notamment d'un helicoptere
US6671593B2 (en) * 1999-12-01 2003-12-30 Sinex Holding Llc Dynamic aircraft maintenance production system
US7076532B2 (en) * 2001-01-15 2006-07-11 Ron Craik System and method for storing and retrieving equipment inspection and maintenance data
US20090083050A1 (en) * 2007-09-25 2009-03-26 Eltman Joseph T Compilation and distribution of data for aircraft fleet management
US7983809B2 (en) * 2007-12-21 2011-07-19 Sikorsky Aircraft Corporation Aircraft integrated support system (ISS)
US8621305B2 (en) 2010-07-08 2013-12-31 Honeywell International Inc. Methods systems and apparatus for determining whether built-in-test fault codes are indicative of an actual fault condition or a false alarm

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4635030A (en) * 1984-07-30 1987-01-06 Canadian Marconi Company Status display system
JP2804125B2 (ja) * 1989-11-08 1998-09-24 株式会社日立製作所 情報処理システムの障害監視装置と制御方法
CA2070834A1 (fr) * 1989-12-07 1991-06-08 Jason Beaufort Scholz Controleur de taux d'erreurs
US5111402A (en) * 1990-01-19 1992-05-05 Boeing Company Integrated aircraft test system
US5138616A (en) * 1990-03-19 1992-08-11 The United States Of America As Represented By The Secretary Of The Army Continuous on-line link error rate detector utilizing the frame bit error rate
US5384565A (en) * 1992-08-03 1995-01-24 Motorola, Inc. Method and apparatus for identifying duplicate data messages in a communication system

Also Published As

Publication number Publication date
FR2715747A1 (fr) 1995-08-04
US5610923A (en) 1997-03-11

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Legal Events

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CD Change of name or company name
TP Transmission of property