The paper presents the lateral acceleration control design of a missile model using the evolution strategy (ES). The nonlinear fixed-structure-like controller is represented by the singleton fuzzy model. This allows a variation of shapes of the gain functions to be explored, and subsequent modification is fairly easy. Instead of finding an optimal decomposition of the fuzzy controller, a set of fuzzy rules is unconventionally optimized for the overall gain surfaces that guarantee acceptable performances for the closed-loop system over the whole operating envelope. The simulation results show that the designed fuzzy gain-scheduled controller is a robust tracking controller for all perturbation vertices


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    Titel :

    Fuzzy gain-scheduled missile autopilot design using evolutionary algorithms


    Beteiligte:
    Screenuch, T. (Autor:in) / Tsourdos, A. (Autor:in) / Hughes, E.J. (Autor:in) / White, B.A. (Autor:in)


    Erscheinungsdatum :

    01.10.2006


    Format / Umfang :

    6224849 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch