Magnetic attitude control for nano-satellites
The active magnetic attitude control technique is a recognized attitude control option for small satellites operated in Low Earth Orbit (LEO). The purpose of this thesis is to control a nano-satellite that is operated in LEO so that it always pointing toward the Earth. Two options of control algorit...
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Format: | Thesis |
Language: | English |
Published: |
2014
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Online Access: | http://eprints.utm.my/id/eprint/48522/1/SyahrimAzhanBinIbrahimMFKE2014.pdf |
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