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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    Titel :

    Dynamic Inversion: An Evolving Methodology for Flight Control Design


    Beteiligte:
    D. Enns (Autor:in) / D. Bugajski (Autor:in) / R. Hendrick (Autor:in) / G. Stein (Autor:in)

    Erscheinungsdatum :

    1995


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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