This paper studies higher order sliding-mode-control laws to deal with some spacecraft-attitude-tracking problems. Quasi-continuous second- and third-order sliding controllers and differentiators are applied to quaternion-based spacecraft-attitude-tracking maneuvers. A class of linear sliding manifolds is selected as a function of angular velocities and quaternion errors. The second method of Lyapunov is used to show that tracking is achieved globally. An example of multiaxial attitude-tracking maneuvers is presented, and simulation results are included to verify and compare the practical usefulness of the various controllers.


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    Title :

    Quasi-continuous higher order sliding-mode controllers for spacecraft-attitude-tracking maneuvers


    Contributors:

    Published in:

    Publication date :

    2010


    Size :

    9 Seiten, 28 Quellen




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English








    Disturbance Accommodating Sliding Mode Controller for Spacecraft Attitude Maneuvers

    Kim, J. / Crassidis, J. L. / American Astronautical Society et al. | British Library Conference Proceedings | 1998