The attitude control of flexible spacecraft

Approved for public release; distribution is unlimited === This thesis details the design of the Naval Postgraduate School's Flexible Spacecraft Simulator and the first attempts at simulation and control of the model. The effect of flexible structures on the attitude control spacecraft has been...

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Bibliographic Details
Main Author: Watkins, R. Joseph
Other Authors: Agrawal, Brij N.
Language:en_US
Published: Monterey, California. Naval Postgraduate School 2013
Online Access:http://hdl.handle.net/10945/26896