Theoretical tools are presented to analyze the relationship between the design choices for a class of NASA-inspired fault-tolerant, reconfigurable computer architectures and the tracking performance degradation of a digital flight control system implemented on such a platform while operating in a high-intensity radiated field (HIRF) environment. A HIRF experiment was conducted at the NASA Langley Research Center to validate the theory for a distributed Boeing 747 flight control system subject to HIRF upsets.


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    Titel :

    Tracking Performance of Distributed Recoverable Flight Control Systems Subject to High Intensity Radiated Fields


    Beteiligte:


    Erscheinungsdatum :

    01.01.2013


    Format / Umfang :

    8432522 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    The NASA High Intensity Radiated Fields Laboratory

    Williams, R. A. / IEEE / AIAA | British Library Conference Proceedings | 1997