These slides describe a method and technology of modeling flexible aircraft for active control of structural dynamics. Objective: Generate models useful for the design and evaluation of control laws for active structural control and flutter suppression that are able to accurately predict body freedom flutter.


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    Title :

    Lessons from Modeling Flexible Aircraft for Active Flutter Suppression


    Contributors:

    Publication date :

    2019


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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