This paper describes a general form of nonlinear dynamic inversion control for use in a generic nonlinear simulation to evaluate condidate augmented aircraft dynamics. The implementation is specifically tailored to the task of quickly assessing an aircraft's control power requirements and defining the achievable dynamic set.


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    Titel :

    Force and Moment Approach for Achievable Dynamics using Nonlinear Dynamics Inversion


    Beteiligte:
    A. J. Ostroff (Autor:in) / B. J. Bacon (Autor:in)

    Erscheinungsdatum :

    1999


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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