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    Fixed structure flight control law design based on genetic algorithm

    Fixed structure flight control law design based on genetic algorithm


    The development of flight control systems using classical control techniques is a costly and time-consuming process. This paper shows how to use genetic algorithm (GA) and modern control techniques to determine the control parameters of the flight control law within the classical structure. An example of designing longitudinal flight control law with the proposed method is presented. The designed flight control law be simulated on a 6 degree-of-freedom nonlinear model of the aircraft.

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    Titel :

    Fixed structure flight control law design based on genetic algorithm

    Beteiligte:
    Feng, Qing-tang (Autor:in) / Jiang, Zhi-hong (Autor:in) / Zhu, Ji-hong (Autor:in) / Liu, Shi-qian (Autor:in)
    Erschienen in:

    CESA, IMACS Multiconference on Computational Engineering in Systems Applications, 2006 ; 1-4

    Erscheinungsdatum :

    2006

    Format / Umfang :

    4 Seiten, 7 Quellen

    ISBN :

    7-900718-14-1

    Medientyp :

    Aufsatz (Konferenz)

    Format :

    Print

    Sprache :

    Englisch

    Schlagwörter :

    Luftraumüberwachung , Regelungssynthese , genetischer Algorithmus , Leistungswert , Raumfahrt

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