Magnetic Attitude Control For Spacecraft with Flexible Appendages
The design of an attitude control system for a flexible spacecraft using magnetic actuation is considered. The nonlinear, linear, and modal equations of motion are developed for a general flexible body. Magnetic control is shown to be instantaneously underactuated, and is only controllable in the ti...
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| Language: | en_ca |
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2012
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| Online Access: | http://hdl.handle.net/1807/33545 |
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