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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    Title :

    Disturbance Observer-Based Attitude Control for Spacecraft With Input MRS


    Contributors:


    Publication date :

    2019-02-01


    Size :

    3684084 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English