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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    Titel :

    Adaptive sliding mode control for missile guidance law


    Beteiligte:
    Wu, Xiangyang (Autor:in) / Bi, Shihua (Autor:in) / Zhu, Zheng (Autor:in) / Wu, Weinan (Autor:in)


    Erscheinungsdatum :

    01.07.2014


    Format / Umfang :

    252473 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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