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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    Title :

    Reconfiguration in an integrated avionics design


    Contributors:
    Seeling, K. (author)


    Publication date :

    1996-01-01


    Size :

    727102 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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