mu -synthesis combines the structured singular value and Hinfinity control to design compensators for plants with structured uncertainty. The application of mu -synthesis to the design of a flight control system for a highly maneuverable tail controlled missile is discussed. Performance goals are given in the time and frequency domains and include time constant, overshoot, stability margins, and high-frequency attenuation. The resulting control law desensitizes the system's performance to structured variations in the missile's aerodynamic properties and provides some robustness, in both a single-loop and a multiloop sense, to variations and/or perturbations not included in the uncertainty model.


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    Titel :

    Applying mu -synthesis to missile autopilot design


    Weitere Titelangaben:

    Autopilot für Flugkörper


    Beteiligte:
    Jackson, P. (Autor:in)


    Erscheinungsdatum :

    1990


    Format / Umfang :

    6 Seiten, 8 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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