Spacecraft attitude control using only magnetic torques is a time-varying system. Many designs have been proposed using linear quadratic regulator (LQR) and H∞ formulations. The existence of the solutions depends on the controllability of the linear time-varying systems, which has not been established. In this paper, the conditions of controllability for this linear time-varying system is derived.


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    Titel :

    Controllability of spacecraft using only magnetic torques


    Beteiligte:
    Yaguang Yang (Autor:in)


    Erscheinungsdatum :

    01.04.2016


    Format / Umfang :

    126076 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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