The problem of missile interception is investigated in this paper. Sliding mode controllers are proposed for the design of guidance laws. Specially, the control design consists of the estimation of the target acceleration by adaptive scheme and thus it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.


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    Title :

    Adaptive sliding mode control for missile guidance law


    Contributors:
    Wu, Xiangyang (author) / Bi, Shihua (author) / Zhu, Zheng (author) / Wu, Weinan (author)


    Publication date :

    2014-07-01


    Size :

    252473 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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