On-orbiting spacecraft are working for a specified long time under the effects of environmental disturbances, uncertainties, component failures, and input saturation.


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    Title :

    Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation


    Contributors:
    Hu, Qinglei (author) / Li, Bo (author) / Xiao, Bing (author) / Zhang, Youmin (author)


    Publication date :

    2021-03-14


    Size :

    36 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English