The attitude consensus control is studied for multiple spacecrafts. Distributed observers for follower systems are constructed to get leader’s state information. The adaptive technique is employed to deal with inertia uncertainties and disturbances. The sliding mode controller(SMC) is constructed based on distributed observers and adaptations to guarantee stability for multiple spacecraft systems. The rigorous proof is given to demonstrate that the errors between followers and the leader are uniformly ultimately bounded (UUB). A numerical simulation is presented to illustrate the performance of the proposed control law.


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    Title :

    Distributed Adaptive Attitude Consensus Control for Multiple Rigid Spacecrafts


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Yu, Xiang (editor) / Qi, Wen-Nian (author) / Wu, Ai-Guo (author) / Dong, Rui-Qi (author)


    Publication date :

    2021-10-30


    Size :

    11 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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