This paper considers the problem of attitude tracking control for uncertain rigid spacecraft subject to control input magnitude and rate saturation (MRS). First, a smooth input MRS model is proposed. Then, a robust attitude tracking control scheme is designed based on the backstepping and finite-time disturbance observer techniques. Finally, the effectiveness of the control scheme derived here is illustrated by numerical simulations.


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    Titel :

    Disturbance Observer-Based Attitude Control for Spacecraft With Input MRS


    Beteiligte:


    Erscheinungsdatum :

    2019-02-01


    Format / Umfang :

    3684084 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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