This paper investigates the integrated orbit and attitude modelling and control problem for on-orbit servicing spacecraft. The integrated relative kinematic and dynamic model for the on-orbit servicing spacecraft and the target is established on the base of dual-quaternion. A backstepping control law is proposed, which is improved then in consideration of system uncertainties. Globally asymptotical stability is analyzed through Lyapunov stability for the closed-loop system. Numerical simulations demonstrate the effectiveness and validity of the proposed methods.


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    Titel :

    Back-stepping based integrated orbit and attitude control for on-orbit servicing spacecraft


    Beteiligte:
    Yueyong Lv (Autor:in) / Ziwei Wang (Autor:in) / Yanning Guo (Autor:in) / Liangming Chen (Autor:in)


    Erscheinungsdatum :

    01.08.2016


    Format / Umfang :

    3297558 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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