Magnetic control for spinning 3-unit science CubeSat
A control system is designed and validated for a 3-unit CubeSat science mission. Utilizing three magnetorquers and one reaction wheel the system achieves a 6 rotation per minute spin rate and orbit normal pointing vector of the long axis of a 3-unit CubeSat. The design is validated across an evoluti...
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| Format: | Others |
| Language: | en |
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2015
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| Online Access: | http://hdl.handle.net/2152/28245 |