A new method of stability margin clearance of missile autopilot is described. First, a model of linear fractional transformation form is established for missile has uncertain parameters; then, the system stability margin requirements are seen as a virtual uncertainty and introduced into the model; Finally, the model is analyzed, and the clearance results about the missile autopilot performance is obtained. The results show this is a more efficient and accurate clearance method than traditional ones.


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    Titel :

    Stability Margin Clearance of Missile Autopilot Using μ Anylysis


    Beteiligte:
    Hou, Zhen-Qian (Autor:in) / Liang, Xiao-Geng (Autor:in) / Wang, Wen-Zheng (Autor:in) / Wang, Qiang-Feng (Autor:in)


    Erscheinungsdatum :

    2012


    Format / Umfang :

    6 Seiten




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Stability Margin Clearance of Missile Autopilot Using μ Anylysis

    Hou, Zhen Qian ;Liang, Xiao Geng ;Wang, Wen Zheng | Trans Tech Publications | 2012





    Multivariable stability margins for missile autopilot coupling

    ARNOLD, III, W. / GATES, N. / WILSON, ARLYNN | AIAA | 1991