This paper examines the problem of introducing advanced forms of fault-tolerance via reconfiguration into safety-critical avionic systems. This is required to enable increased availability after fault occurrence in distributed integrated avionic systems (compared to static federated systems). The approach taken is to identify a migration path from current architectures to those that incorporate re-configuration to a lesser or greater degree. Other challenges identified include change of the development process; incremental and flexible timing and safety analyses; configurable kernels applicable for safety-critical systems.


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    Titel :

    Distributed fault-tolerant avionic systems-a real-time perspective


    Beteiligte:
    Audsley, N.C. (Autor:in) / Burke, M. (Autor:in)


    Erscheinungsdatum :

    01.01.1998


    Format / Umfang :

    1966632 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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