The main feature of the exiting attitude control approaches can only achieve the steady-state performance. The transient control performance can not be determined or prescribed. This is an important performance index in the practical satellite mission. To achieve satellite attitude maneuvering with external disturbances, performance constraint, and actuator fault [1], an adaptive FTC law was designed via the prescribed performance control (PPC) technique.


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    Title :

    Fixed-Time Optimal Attitude Control


    Contributors:
    Xiao, Bing (author) / Chen, Zhaoyue (author) / Xu, Jingwen (author) / Cao, Lu (author)

    Published in:

    Publication date :

    2024-07-03


    Size :

    19 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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