Automatic digital electronic control system based on inverse-model-follower concept being developed for proposed vertical-attitude-takeoff-and-landing airplane. Inverse-model-follower control places inverse mathematical model of dynamics of controlled plant in series with control actuators of controlled plant so response of combination of model and plant to command is unity. System includes feedback to compensate for uncertainties in mathematical model and disturbances imposed from without.


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    Title :

    Automatic Flight Controller With Model Inversion


    Contributors:

    Published in:

    Publication date :

    1992-07-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Aircraft automatic flight control system with model inversion

    Smith, G. Allan / Meyer, George | NTRS | 1987


    Aircraft automatic flight control system with model inversion

    SMITH, G. ALLAN / MEYER, GEORGE | AIAA | 1987


    Aircraft automatic flight control system with model inversion

    Smith, G. A. / Meyer, George | NTRS | 1990