Initial guess and optimization strategies for multi-body space trajectories with application to free return trajectories to near-Earth asteroids
This concept of calculating, optimizing, and utilizing a trajectory known as a ``Free Return Trajectory" to facilitate spacecraft rendezvous with Near-Earth Asteroids is presented in this dissertation. A Free Return Trajectory may be defined as a trajectory that begins and ends near the same p...
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| Format: | Others |
| Language: | en |
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2014
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| Online Access: | http://hdl.handle.net/2152/26858 |