Abstract In this chapter, an adaptive fast terminal sliding mode control law (AFTSMCL) is presented to resolve attitude tracking control problem for rigid spacecraft, which can provide finite-time convergence, strong robustness, and fault-tolerant control. A rigorous proof is achieved first. Simulation results are presented to illustrate the effectiveness of presented control law.


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    Title :

    Finite-Time Tracking Control of Rigid Spacecraft Under Actuator Saturations and Faults


    Contributors:
    Xia, Yuanqing (author) / Zhang, Jinhui (author) / Lu, Kunfeng (author) / Zhou, Ning (author)


    Publication date :

    2018-07-03


    Size :

    29 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English