The use of solutions to problems of spacecraft trajectory optimization in impulse formulation when solving the problems of optimal control of trajectories of a spacecraft with limited thrust engine: I

Author： Grigoriev I.   Grigoriev K.  

Publisher： MAIK Nauka/Interperiodica

ISSN： 0010-9525

Source： Cosmic Research, Vol.45, Iss.4, 2007-08, pp. : 339-347

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