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

    Kongress:

    AIAA/ASME/ASCE/AHS 24th Struct., Struct. Dyn. and Mater. Conf. ; 1983 ; Lake Tahoe, NV, United States


    Erscheinungsdatum :

    01.03.1983


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Design of the Flutter Suppression System for Dast Arw-IR

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


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

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


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

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