Method of characteristic constants and retro- thrust optimality in agravitational field - necessary and sufficient conditions
Aerospace Sciences Meeting ; 1964 ; New York , NY , U.S.A.
1964-01-01
Conference paper
Electronic Resource
English
AIAA-2002-4726 Second-Order Necessary and Sufficient Conditions Applied to Low-Thrust Trajectories
British Library Conference Proceedings | 2002
|American Institute of Physics | 2017
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