The approach to an analytical study of flexible airplane longitudinal handling qualities was to parametrically vary the natural frequencies of two symmetric elastic modes to induce mode interactions with the rigid body dynamics. Since the structure of the pilot model was unknown for such dynamic interactions, the optimal control pilot modeling method is being applied and used in conjunction with pilot rating method.


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    Title :

    Handling Qualities of Large Flexible Control-Configured Aircraft


    Contributors:
    R. L. Swaim (author)

    Publication date :

    1979


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English