In this paper, finite-time fault-tolerant attitude tracking control is investigated for rigid spacecraft system with external disturbances, inertia uncertainties and actuator faults. A novel finite-time disturbance observer combined with a nonsingular terminal sliding mode controller is developed. Using an equivalent output error injection approach, a finite-time disturbance observer with simple structure is firstly designed to estimate lumped uncertainty. Then, to remove the requirement of prior knowledge about lumped uncertainty and reduce chattering, an adaptive finite-time disturbance observer is further proposed, and the estimations converge to the neighborhood of the true values. Based on the designed observer, a unified finite-time attitude controller is obtained automatically. Finally, both additive and multiplicative faults are considered for simulations and the results illustrate the great fault-tolerant capability of the proposed scheme.


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    Titel :

    Disturbance observer-based fault-tolerant attitude tracking control for rigid spacecraft with finite-time convergence


    Beteiligte:
    Zong, Qun (Autor:in) / Zhang, Xiuyun (Autor:in) / Shao, Shikai (Autor:in) / Tian, Bailing (Autor:in) / Liu, Wenjing (Autor:in)


    Erscheinungsdatum :

    2019-02-01


    Format / Umfang :

    13 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch