Abstract This paper considers the attitude and angular velocity stabilization problem of a class of flexible spacecraft under actuator complete failure. Firstly a new model simplification strategy is put forward to weaken the coupling effects. Then an adaptive observer-based estimation method is proposed to estimate the uncertainty of flexibility, based on which a feedback fault-tolerant control scheme is further developed which guarantees the system stability and asymptotic attitude converging properties. The simulation results illustrate the efficiency of the theoretical results.


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    Titel :

    Attitude stabilization of a flexible spacecraft under actuator complete failure


    Beteiligte:
    Zhao, Dong (Autor:in) / Yang, Hao (Autor:in) / Jiang, Bin (Autor:in) / Wen, Liyan (Autor:in)

    Erschienen in:

    Acta Astronautica ; 123 ; 129-136


    Erscheinungsdatum :

    2016-02-23


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch