Hybrid Magnetic Attitude Controller for Low Earth Orbit Satellites using the Time-varying Linear Quadratic Regulator
The following is a study of an attitude control system (ACS) for a low earth orbit nanosatellite. Control actuation is applied using three reaction wheels and three mutually orthogonal current-driven magnetorquers which produce torques by interacting with the earth’s magnetic field. Control torques...
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| Language: | en_ca |
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2009
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| Online Access: | http://hdl.handle.net/1807/17711 |