The purpose of this study was to design and test a failure detection and isolation subsystem for a triply redundant asychronous digital flight control system. The focus of the research was to analyze the time skew effect in an asychronous environment. A model to estimate the time skew and the time skew related interchannel difference was developed. The design was tested in a simulation environment where the YF-16 longitudinal dynamics and the AFTI/F-16 digital flight control system were modelled.


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    Titel :

    Failure Detection and Isolation for an Asychronous Digital Flight Control System


    Beteiligte:
    G. Serpen (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    192 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch