Usually the missile attitude control process in a large flight envelope has strong time-varying and nonlinear characteristics, so the controller parameter is difficultly scheduled with conventional PID control approach. In this study a linear active disturbance rejection control approach based on reduced-order linear extended state observer is proposed. The approach is employed to the attitude controller for a supersonic missile in attack with high angle. It is not hard to determine the proposed controller parameter, and the numeral simulations show that the presented approach has a very good capability on tracking attitude command.


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    Titel :

    Missile attitude control in a large flight envelope based on the linear active disturbance rejection control approach


    Beteiligte:
    Hui, Li (Autor:in) / Yu, Fan (Autor:in) / Fengyi, Li (Autor:in) / Chuang, Song (Autor:in) / Zhide, Yin (Autor:in)


    Erscheinungsdatum :

    2014-08-01


    Format / Umfang :

    123717 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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