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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    Titel :

    One-axis attitude of arbitrary satellite using magnetorquers only


    Beteiligte:

    Erschienen in:

    Cosmic Research ; 51 , 6 ; 478-484


    Erscheinungsdatum :

    01.11.2013


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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