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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    Title :

    Force and Moment Approach for Achievable Dynamics using Nonlinear Dynamics Inversion


    Contributors:
    A. J. Ostroff (author) / B. J. Bacon (author)

    Publication date :

    1999


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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