Discussed is the technology of active flutter suppression research by the use of the wind-tunnel model of a delta wing with low aspect ratio. The research includes the establishment of a mathematical model for the servo-aeroelastic system, and the synthesis and analysis of sub-optimal output feedback control laws for active flutter suppression.


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    Title :

    Investigation of Control Law for Active Flutter Suppression


    Contributors:
    W. Wang (author) / Z. Gu (author) / D. Zhu (author)

    Publication date :

    1987


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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