The potential of Hybrid Phase Stabilization (HPS), particularly for highly unstable aircraft, using a hypersonic flight vehicle (HSV) as a relevant example, is discussed. The development of HPS is presented and the result is compared with that generated using a conventional gain stabilization technique. Since HPS was not addressed in the MIL-spec requirements, a preliminary residual response metric was developed to provide guidance in assessing HPS.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aeroservoelastic stabilization techniques 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) / Mcrue, Duane T. (Autor:in)

    Erscheinungsdatum :

    1991-12-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    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

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


    Aeroservoelastic stabilization technique refinement for hypersonic flight vehicles

    Cheng, Peter Y. / Chan, Samuel Y. / Myers, Thomas T. et al. | NTRS | 1992


    Aeroservoelastic stabilization technique refinement for hypersonic flight vehicles

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