For on-orbiting spacecraft, FTC and CA techniques are generally utilized to ensure the stability, reliability, autonomy and intelligence, and the percentage of successfully accomplished missions of the spacecraft ACS, especially in the presence of external disturbances, actuator constraints and faults.


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    Title :

    Conclusions


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

    Published in:

    Publication date :

    2021-03-14


    Size :

    3 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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