An active flutter control methodology based on linear quadratic gaussian theory and its application to the control of a super critical wing is presented. Results of control surface and sensor position optimization are discussed. Both frequency response matching and residualization used to obtain practical flutter controllers are examined. The development of algorithms and computer programs for flutter modeling and active control design procedures is reported.


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    Title :

    Active flutter control for flexible vehicles, volume 1


    Contributors:

    Publication date :

    1979-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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