Conventional gain-stabilization techniques introduce low frequency effective time delays which can be troublesome from the viewpoint of SSTOV vehicles' flying qualities. These time delays can be alleviated through a blending of gain-stabilization and phase-stabilization techniques; the resulting hybrid phase stabilization (HPS) for the low-frequency structural modes has been noted to have greater residual response than a conventional gain-stabilizer design. HPS design procedures are presently refined, and residual response metrics are developed.


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    Titel :

    Aeroservoelastic stabilization technique refinement for hypersonic flight vehicles


    Beteiligte:
    Cheng, Peter Y. (Autor:in) / Chan, Samuel Y. (Autor:in) / Myers, Thomas T. (Autor:in) / Klyde, David H. (Autor:in) / Mcruer, Duane T. (Autor:in)

    Kongress:

    AIAA, International Aerospace Planes Conference ; 1992 ; Orlando, FL, United States


    Erscheinungsdatum :

    01.12.1992


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Aeroservoelastic stabilization technique refinement for hypersonic flight vehicles

    CHENG, PETER / CHAN, SAMUEL / MYERS, THOMAS et al. | AIAA | 1992


    Aeroservoelastic stabilization techniques for hypersonic flight vehicles

    CHENG, PETER / CHAN, SAMUEL / MYERS, THOMAS et al. | AIAA | 1991


    Aeroservoelastic stabilization techniques for hypersonic flight vehicles

    Chan, Samuel Y. / Cheng, Peter Y. / Pitt, Dale M. et al. | NTRS | 1991


    Aeroservoelastic stabilization techniques for hypersonic flight vehicles

    Cheng, Peter Y. / Chan, Samuel Y. / Myers, Thomas T. et al. | NTRS | 1991


    Aeroservoelastic Stabilization Techniques for Hypersonic Flight Vehicles

    S. Y. Chan / P. Y. Cheng / D. M. Pitt et al. | NTIS | 1991