In the future, large satellites may be automatically assembled on-orbit in order to reduce weight and increase volume efficiency in launchers. During this process, it may be important to maintain satellite attitude. This paper presents a dynamic model, including reaction wheels and a twisting-algorithm-based sliding-mode controller, to maintain attitude during a simple self-assembly process. Simulation results of this controller are compared with results from other controllers found in the literature.


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    Titel :

    Robust control for satellite attitude regulation during on-orbit assembly


    Beteiligte:


    Erscheinungsdatum :

    01.02.2016


    Format / Umfang :

    3185610 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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