This note investigates the finite-time attitude control problems for a single spacecraft and multiple spacecraft. First of all, a finite-time controller is designed to solve finite-time attitude tracking problem for a single spacecraft. Rigorous proof shows that the desired attitude can be tracked in finite time in the absence of disturbances. In the presence of disturbances, the tracking errors can reach a region around the origin in finite time. Then, based on the neighbor rule, a distributed finite-time attitude control law is proposed for a group of spacecraft with a leader-follower architecture. Under the finite-time control law, the attitude synchronization can be achieved in finite time.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization


    Beteiligte:
    Du, Haibo (Autor:in) / li, Shihua (Autor:in) / Qian, Chunjiang (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2011


    Format / Umfang :

    7 Seiten, 21 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Decentralized Finite-Time Attitude Synchronization and Tracking Control for Rigid Spacecraft

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


    Quaternion-based finite time control for spacecraft attitude tracking

    Wu, Shunan / Radice, Gianmarco / Gao, Yongsheng et al. | Elsevier | 2011


    Finite-Time Attitude Trajectory Tracking Control of Rigid Spacecraft

    Xiao-Ning Shi, / Zhi-Gang Zhou, / Di Zhou, | IEEE | 2017