The problem of designing flight control system for high performance anti-air missiles is discussed in this report. The research addresses three areas of missile autopilot design. The first area investigates the application of nonlinear H-infinity optimal control for an integrated aerodynamic/thrust vector controlled missile. The second area investigates the design of autopilots for missiles using on-off reaction control valve actuators. A sliding mode control law is developed using H-infinity design methods. The third area focused on developing nonconservative robustness analysis algorithms for gain scheduled missile autopilots.


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    Titel :

    Nonlinear Control of Missiles


    Beteiligte:
    K. A. Wise (Autor:in) / J. L. Sedwick (Autor:in) / R. L. Eberhardt (Autor:in)

    Erscheinungsdatum :

    1995


    Format / Umfang :

    196 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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