A technique is proposed which will make the flight director computer performance independent of aircraft dynamics, wind or aircraft position relative to the navigation beam. The control law proposed will compensate for all such variables with an error correcting mechanism. This technique results in a computer that is universal in its application.


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    Title :

    A Universal Flight Director Computer


    Contributors:

    Publication date :

    1974


    Size :

    60 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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