Spacecraft missions usually require precise operations under limited fuel consumption. In this chapter, for the short-range relative motion of on-orbit service spacecraft during rendezvous and docking missions, we will improve control accuracy, reducing energy consumption, and optimizing the travel distance through time-synchronized control. Finite-time and fixed-time-synchronized controllers are proposed to drive the relative attitude or orbit tracking error to the origin synchronously within the finite or fixed time. Time-synchronized convergence of all the state elements of the 6-DOF spacecraft is achieved, while the merits of shortening the travel length of the output and saving fuel consumption are revealed.


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    Titel :

    Time-Synchronized Spacecraft Control in Rendezvous and Docking


    Beteiligte:
    Li, Dongyu (Autor:in) / Ge, Shuzhi Sam (Autor:in) / Lee, Tong Heng (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2022-01-10


    Format / Umfang :

    32 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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