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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    Title :

    Aircraft Load Factor Overload Warning Systems


    Contributors:

    Publication date :

    1980


    Size :

    15 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Aircraft Load Factor Overload Warning System

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


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