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.


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    Titel :

    Aeroservoelastic Stabilization Techniques for Hypersonic Flight Vehicles


    Beteiligte:
    S. Y. Chan (Autor:in) / P. Y. Cheng (Autor:in) / D. M. Pitt (Autor:in) / T. T. Myers (Autor:in) / D. H. Klyde (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    95 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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