A control law is developed to suppress symmetric flutter for a mathematical model of an aeroelastic research vehicle. An implementable control law is attained by including modified LQC (Linear Quadratic Gaussian) design techniques, controller order reduction, and gain scheduling. An alternate (complementary) design approach is illustrated for one flight condition wherein nongradient-based constrained optimization techniques are applied to maximize controller robustness.


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    Title :

    Design of a Candidate Flutter Suppression Control Law for DAST ARW-2


    Contributors:
    W. M. Adams (author) / S. H. Tiffany (author)

    Publication date :

    1984


    Size :

    28 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Design of a candidate flutter suppression control law for DAST ARW-2

    Adams, W. M., Jr. / Tiffany, S. H. | NTRS | 1983



    Design of a candidate flutter suppression control law for DAST ARW-2

    Adams, W. M., Jr. / Tiffany, S. H. | NTRS | 1984


    Design of the flutter suppression system for DAST ARW-IR

    Newsom, J. R. / Pototzky, A. S. / Abel, I. | NTRS | 1983


    Design of the Flutter Suppression System for Dast Arw-IR

    J. R. Newsom / A. S. Pototzky / I. Abel | NTIS | 1983