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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    Title :

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


    Contributors:
    Yueyong Lv, (author) / Ziwei Wang, (author) / Yanning Guo, (author) / Liangming Chen, (author)


    Publication date :

    2016-08-01


    Size :

    3297558 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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