A novel approach combining the sliding mode control (SMC) and extended state observer (ESO) is proposed for attitude control of an early warning satellite model which is non-linear in dynamics. The sliding mode controller is designed to guarantee the state variables of the closed-loop system to converge to the reference state with the help of the ESO by estimating the unknown disturbance. Then, simulation results illustrate the effectiveness of the control strategy.


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    Titel :

    Early warning satellite attitude SMC base on ESO


    Beteiligte:
    Cong, Zhang (Autor:in) / Yunjie, Wu (Autor:in) / Jingxing, Zuo (Autor:in)


    Erscheinungsdatum :

    01.08.2014


    Format / Umfang :

    351384 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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