To study the effectiveness of various control system design methodologies, the NASA Langley Research Center initiated the Benchmark Active Controls Project. In this project, the various methodologies were applied to design a flutter suppression system for the Benchmark Active Controls Technology (BACT) Wing. This report describes the user's manual and software toolbox developed at the University of Washington to design a multirate flutter suppression control law for the BACT wing.


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    Title :

    Multirate Flutter Suppression System Design for the Benchmark Active Controls Technology Wing


    Contributors:

    Publication date :

    2002-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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