Abstarct An active magnetic control synthesis for attitude guidance of “Chibis-M” microsatellite is considered. The only information required is the data from the sun sensor. Applicability of a control to achieve solar panels sun-pointing is studied. Equations of motions are analytically solved using averaging technique. The behavior of a system with respect to initial conditions and orbit parameters is studied.


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    Title :

    One-axis attitude of arbitrary satellite using magnetorquers only


    Contributors:

    Published in:

    Cosmic Research ; 51 , 6 ; 478-484


    Publication date :

    2013-11-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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