The design of the flutter suppression system for a remotely-piloted research vehicle is described. The modeling of the aeroelastic system, the methodology used to synthesized the control law, the analytical results used to evaluate the control law performance, and ground testing of the flutter suppression system onboard the aircraft are discussed. The major emphasis is on the use of optimal control techniques employed during the synthesis of the control law.


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    Titel :

    Design of the Flutter Suppression System for Dast Arw-IR


    Beteiligte:
    J. R. Newsom (Autor:in) / A. S. Pototzky (Autor:in) / I. Abel (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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


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    Design of the flutter suppression system for DAST ARW-1R - A status report

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



    Design of the flutter suppression system for DAST ARW-1R - A status report

    NEWSOM, J. / ABELT, I. / POTOTZKY, A. | AIAA | 1983