Classical Element Feedback Control for Spacecraft Orbital Maneuvers
The recent addition of autonomous formation flying spacecraft to the world's satellite fleet provides new motivation to study feedback control techniques. In this thesis, we develop nonlinear orbit control laws for use in spacecraft orbital maneuvers, and spacecraft formation flying. We apply...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/33354 http://scholar.lib.vt.edu/theses/available/etd-05312002-124715/ |