Redundancy requirements and trade-off criteria are established for flight critical digital flight control systems with particular emphasis on the fly-by-wire application. The use of general purpose digital computers is considered, with self-test and cross-channel comparison monitoring techniques to obtain the necessary flight safety reliability. A reliability model is presented which includes the effects of detected and undetected failures and provides a basis for establishing in-flight and preflight test coverage requirements consistent with a given reliability goal.


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    Titel :

    Digital Flight Control System Redundancy Study


    Beteiligte:
    J. McGough (Autor:in) / K. Moses (Autor:in) / W. Platt (Autor:in) / G. Reynolds (Autor:in) / J. Strole (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    341 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch