Upon aircraft landing approach, flare path command signals of altitude, vertical velocity and vertical acceleration are generated as functions of aircraft position and velocity with respect to the ground. The command signals are compared with corresponding actual values to generate error signals which are used to control the flight path.


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    Title :

    Aircraft landing control system


    Contributors:

    Publication date :

    1982-11-02


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English