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, Part 2


    Beteiligte:
    G. S. Mason (Autor:in) / M. C. Berg (Autor:in) / V. Mukhopadhyay (Autor:in)

    Erscheinungsdatum :

    2002


    Format / Umfang :

    47 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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

    Mason, Gregory S. / Berg, Martin C. / Mukhopadhyay, Vivek | NTRS | 2002


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

    Mason, Gregory S. / Berg, Martin C. / Mukhopadhyay, Vivek | NTRS | 2002



    Multirate flutter suppression system design for a model wing

    Mason, Gregory S. / Berg, Martin C. | AIAA | 1994