This paper studies a novel robust adaptive finite-time attitude tracking and synchronization control problem for multi-spacecraft with leader-following architecture, actuator saturation, unknown time-varying inertia and disturbance. Aiming at rejecting the influence of uncertainties and disturbances, an adaptive algorithm is proposed with no prior knowledge of inertia. Meanwhile, based on finite-time control, consensus algorithm and graph theory, a robust adaptive and synchronized attitude tracking control law with a dynamic adjustment function is presented to regulate the attitude to a common time-varying desired state in finite time and improve the dynamic property of system. The effectiveness and performance of the designed control approach are demonstrated through numerical simulation results.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Robust adaptive finite-time attitude tracking and synchronization control for multi-spacecraft with actuator saturation


    Contributors:
    Zhu, Zhihao (author) / Guo, Yu (author)


    Publication date :

    2019-02-01


    Size :

    12 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English






    Finite-Time Fault Tolerant Attitude Tracking Control for Rigid Spacecraft with Actuator Saturation

    Xia, Yuanqing / Zhang, Jinhui / Lu, Kunfeng et al. | Springer Verlag | 2018



    Adaptive Spacecraft Attitude Tracking Control with Actuator Uncertainties

    Yoon, H. / Tsiotras, P. / American Astronautical Society; American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008