This paper addresses the problem of switching performance optimal control for the longitudinal model of the generic hypersonic air-breathing flight vehicle. For the widening flight envelope of hypersonic vehicle, the multiple-mode switching control is an issue that have to be considered. The approach presented makes use of the bumpless transfer technique and gives a switching performance optimal controller design method for coping with bumps and undesirable transients in multiple-mode switching systems. Simulation results for the generic hypersonic vehicle model show the effectiveness of the proposed design method.


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    Titel :

    Switching performance optimal controller design for hypersonic vehicle model


    Beteiligte:
    Yiwen Qi, (Autor:in) / Wen Bao, (Autor:in)


    Erscheinungsdatum :

    01.06.2010


    Format / Umfang :

    794168 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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