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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    Titel :

    Investigation of control law for active flutter suppression


    Beteiligte:
    Wang, Weipeng (Autor:in) / Gu, Zhongquan (Autor:in) / Zhu, Demao (Autor:in)

    Erscheinungsdatum :

    01.11.1987


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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