Geodesic
Analytical solution of equations of near-circular spacecraft's orbit orientation
Izvestiya of Saratov University. Mathematics. Mechanics. Informatics, Tome 15 (2015) no. 1, pp. 97-105.

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The problem of optimal reorientation of spacecraft's orbit with a limited control, orthogonal to the plane of spacecraft's orbit, is considered. An approximate analytical solution of differential equations of near-circular spacecraft's orbit orientation by control, that is permanent on adjacent parts of the active spacecraft's motion, is obtained. 
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I. A. Pankratov. Analytical solution of equations of near-circular spacecraft's orbit orientation. Izvestiya of Saratov University. Mathematics. Mechanics. Informatics, Tome 15 (2015) no. 1, pp. 97-105. http://geodesic.mathdoc.fr/item/ISU_2015_15_1_a13/

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