In this paper a systematic approach for weight selection has been applied. A classical phase lead compensator is used as weight (precompensator) in H infinity loop shaping for design of pitch controller for air vehicle. Analysis has been confined only to bode plots. The analysis and results achieved indicate that H infinity loop shaping control theory is a viable tool for design and synthesis of attitude control of air vehicle.


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    Titel :

    Weight selection in H- infinity loop shaping using lead/lag compensators


    Beteiligte:
    Ejaz, M. (Autor:in) / Arbab, M.N. (Autor:in) / Shah, S.W. (Autor:in)


    Erscheinungsdatum :

    2006


    Format / Umfang :

    6 Seiten, 8 Quellen



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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