An overload warning system for fighter type aircraft combines analytical techniques of computing structural loads with flight conditions and aircraft control inputs to calculate the allowable load factor/control input on a real time basis. The flight conditions and aircraft control inputs are monitored by a microprocessor, which continuously monitors actual load factor, compares the answers with a computed allowable value and generates an ouput signal whenever a prescribed value is exceeded. This signal is available for transmission to aural or visual warning devices and for permanent recording. (Author)


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    Titel :

    Aircraft Load Factor Overload Warning System


    Beteiligte:
    J. T. Johnston (Autor:in) / G. W. Venorsky (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    5 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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