This paper describes nonlinear dynamic inversion as an alternative design method for flight controls. The method is illustrated with super-maneuvering control laws for the F-18 High Angle-of-Attack Research Vehicle (HARV).


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    Title :

    Dynamic Inversion: An Evolving Methodology for Flight Control Design


    Contributors:
    D. Enns (author) / D. Bugajski (author) / R. Hendrick (author) / G. Stein (author)

    Publication date :

    1995


    Size :

    12 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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