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 output 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 Systems


    Beteiligte:
    J. J. Johnston (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Aircraft Load Factor Overload Warning System

    J. T. Johnston / G. W. Venorsky | NTIS | 1980


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