Design and optimization of body-to-body impulsive trajectories in restricted four-body models
Spacecraft trajectory optimization is a topic of crucial importance to space missions design. The less fuel required to accomplish the mission, the more payload that can be transported, and the higher the opportunity to lower the cost of the space mission. The objective is to find the optimal trajec...
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| Format: | Others |
| Language: | English |
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2012
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| Online Access: | http://hdl.handle.net/2152/ETD-UT-2010-12-2370 |