Abstract The attitude stabilization problem for rigid spacecraft in the presence of inertial uncertainties, external disturbances, actuator saturations, and actuator faults is addressed in this chapter. First, a novel fast terminal sliding mode manifold is designed to avoid the singularity problem while providing high control ability. In addition, fast terminal sliding mode control laws are proposed to make the spacecraft system trajectory fast converge onto the fast terminal sliding mode surface, and finally evolve into a small region in finite time, which cannot be achieved by the previous literatures. Based on the real sliding mode context, a practical adaptive fast terminal sliding mode control law is presented to guarantee attitude stabilization in finite time. Also, simulation results are presented to illustrate the effectiveness of the control strategies.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Adaptive Finite-Time Attitude Stabilization for Rigid Spacecraft with Actuator Faults and Saturation Constraints


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


    Erscheinungsdatum :

    03.07.2018


    Format / Umfang :

    22 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Finite-time fault-tolerant attitude stabilization for spacecraft with actuator saturation

    Qiang Shen / Danwei Wang / Senqiang Zhu et al. | IEEE | 2015


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

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


    Finite-Time Attitude Stabilization for Rigid Spacecraft

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


    Adaptive Compensation Control for Spacecraft Attitude Stabilization with Actuator Misalignment and Faults

    Xiao, B. / Hu, Q. / Singhose, W. et al. | British Library Conference Proceedings | 2012