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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Bibliographic Details
Main Author: Ibrahim, Syahrim Azhan
Format: Thesis
Language:English
Published: 2014
Subjects:
Online Access:http://eprints.utm.my/id/eprint/48522/1/SyahrimAzhanBinIbrahimMFKE2014.pdf
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