The application of the self-tuning regulator concept to adaptively control aircraft wing/store flutter instability is described. A simple design based on a reduced-order aircraft model has been successfully tested on a high-order simulation of an advanced aircraft, and performance was found to be comparable to another design using on-line maximum likelihood identification of plant parameters. The main advantage of the self-tuning regulator is its simplicity, while the main disadvantage is the inadequacy of prior performance guarantees.


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    Title :

    Self-tuning regulator design for adaptive control of aircraft wing/store flutter


    Contributors:
    Johnson, T. L. (author) / Harvey, C. A. (author) / Stein, G. (author)


    Publication date :

    1982-10-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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