A Method for Solving the Multi-Extreme Problem of Optimizing Trajectories of a Spacecraft with an Elecrto-Jet Propulsion System’s Thrust
1949 ◽
Vol 28
(4)
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pp. 149
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Keyword(s):
1991 ◽
Vol 36
(3)
◽
pp. 385-394
◽
Keyword(s):