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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    Title :

    Switching performance optimal controller design for hypersonic vehicle model


    Contributors:
    Yiwen Qi, (author) / Wen Bao, (author)


    Publication date :

    2010-06-01


    Size :

    794168 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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