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.
One-axis attitude of arbitrary satellite using magnetorquers only
Cosmic Research ; 51 , 6 ; 478-484
01.11.2013
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
One-axis attitude of arbitrary satellite using magnetorquers only
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