Geodesic
Analytical solution of differential equations of circular spacecraft orbit orientation
Izvestiya of Saratov University. Mathematics. Mechanics. Informatics, Tome 11 (2011) no. 1, pp. 84-89

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The problem of optimal reorientation of spacecraft's orbit with a limited control, orthogonal to the plane of spacecraft orbit is being investigated. We have found an analytical solution of differential equations of circular spacecraft orbit orientation by control that is permanent on adjacent parts of the active spacecraft's motion. 
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I. A. Pankratov; Yu. N. Chelnokov. Analytical solution of differential equations of circular spacecraft orbit orientation. Izvestiya of Saratov University. Mathematics. Mechanics. Informatics, Tome 11 (2011) no. 1, pp. 84-89. http://geodesic.mathdoc.fr/item/ISU_2011_11_1_a10/