Six degree of freedom optimal trajectories for satellite rendezvous
<p>A method is developed for computing the minimum fuel trajectory for a satellite that moves between two different positions and orientations using a sequence of impulsive burns. The method makes use of the linear Clohessy-Wiltshire equations to describe translational motions, Euler's eq...
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| Format: | Others |
| Language: | en |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/41037 http://scholar.lib.vt.edu/theses/available/etd-02132009-171146/ |