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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    Titel :

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


    Beteiligte:

    Erscheinungsdatum :

    01.12.2002


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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