An Investigation of Nonlinear Control of Spacecraft Attitude
The design of controllers subject to the nonlinear H-infinity criterion is explored. The plants to be controlled are the attitude motion of spacecraft, subject to some disturbance torque. Two cases are considered: the regulation about an inertially-fixed direction, and an Earth-pointing spacecraft i...
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| Language: | en_ca |
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2013
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| Online Access: | http://hdl.handle.net/1807/42688 |
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