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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    Title :

    Controllability of spacecraft using only magnetic torques


    Contributors:


    Publication date :

    2016-04-01


    Size :

    126076 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English