Evaluation of energy-sink stability criteria for dual-spin spacecraft
Approved for public release; distribution is unlimited === The nutational stability of a dual-spin, quasi-rigid, axisymmetric spacecraft containing a driven rotor is analyzed. The purpose is to examine a revised energy-sink stability theory that properly accounts for the energy contribution of the m...
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| Language: | en_US |
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Monterey, California. Naval Postgraduate School
2013
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| Online Access: | http://hdl.handle.net/10945/28185 |