Design of a control law for simultaneously suppressing the symmetric and antisymmetric flutter modes of a string mounted fixed-in-roll aeroelastic wind tunnel model is described. The flutter suppression control law was designed using linear quadratic Gaussian theory and involved control law order reduction, a gain root-locus study, and the use of previous experimental results. A 23 percent increase in open-loop flutter dynamic pressure was demonstrated during the wind tunnel test. Rapid roll maneuvers at 11 percent above the symmetric flutter boundary were also performed when the model was in a free-to-roll configuration.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Flutter Suppression Digital Control Law Design and Testing for the Afw Wind-Tunnel Model


    Contributors:

    Publication date :

    1992


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English