This paper continues the study of the problem on determination of parameters of the spherical motion of a spacecraft and control of this motion using only the Earth magnetic field. The problem of damping the angular velocity of this spacecraft and construction of three-axis orientation regime is solved. An algorithm for estimation of parameters of the spherical motion, which has a wide region of convergence, is proposed.


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    Title :

    Control of the spherical motion of a spacecraft in the Earth magnetic field. II. Orientation and stabilization


    Contributors:

    Published in:

    Publication date :

    1998


    Size :

    3 Seiten, 17 Quellen



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English






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