In this paper a novel terminal guidance law for hypersonic vehicle is investigated. In order to accelerate the convergence rate of line of sight angle, adding a power integrator technique based nonlinear guidance law which can make the line of sight converge to zero in finite time is proposed. Then rigorous stability analysis of finite-time convergence is shown. It demonstrates the effectiveness of the approach by numerical simulation meanwhile the approach have strong robustness in the presence of disturbance.


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    Titel :

    Adding a power integrator technique based terminal guidance law


    Beteiligte:
    Wang, Songyan (Autor:in) / Sun, Xiangyu (Autor:in) / Chao, Tao (Autor:in) / Ma, Ping (Autor:in)


    Erscheinungsdatum :

    01.08.2016


    Format / Umfang :

    206231 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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