Abstract In this chapter, an adaptive fast terminal sliding mode control law (AFTSMCL) is presented to resolve attitude tracking control problem for rigid spacecraft, which can provide finite-time convergence, strong robustness, and fault-tolerant control. A rigorous proof is achieved first. Simulation results are presented to illustrate the effectiveness of presented control law.


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    Titel :

    Finite-Time Tracking Control of Rigid Spacecraft Under Actuator Saturations and Faults


    Beteiligte:
    Xia, Yuanqing (Autor:in) / Zhang, Jinhui (Autor:in) / Lu, Kunfeng (Autor:in) / Zhou, Ning (Autor:in)


    Erscheinungsdatum :

    03.07.2018


    Format / Umfang :

    29 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch







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

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


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