This report covers the subject of F-22 avionics core processing fault tolerance and reconfiguration. Fault tolerance is defined as a survivable attribute of a system that allows it to deliver its expected service after faults have manifested themselves within the system. The report addresses all dimensions of the integrated avionics processing fault tolerance/reconfiguration implementation. This includes the preparation for failures, detection of failures, determination and implementation of a recovery scheme, and return to operations.


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    Titel :

    Reconfiguration in an integrated avionics design


    Beteiligte:
    Seeling, K. (Autor:in)


    Erscheinungsdatum :

    01.01.1996


    Format / Umfang :

    727102 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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