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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    Title :

    Aeroservoelastic Stabilization Techniques for Hypersonic Flight Vehicles


    Contributors:
    S. Y. Chan (author) / P. Y. Cheng (author) / D. M. Pitt (author) / T. T. Myers (author) / D. H. Klyde (author)

    Publication date :

    1991


    Size :

    95 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    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

    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 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