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Optimal injection of a satellite into geostationary orbit using a limited number of thruster firings. (English. Russian original) Zbl 1311.49099

J. Comput. Syst. Sci. Int. 52, No. 6, 938-948 (2013); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upr. 2013, No. 6, 97-107 (2013).
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