Attitude control for a nano-satellite
Nano-satellites are classified as satellites weighing less than 20kg. This dissertation presents the design and development of an Attitude Control System (ACS) for a nanosatellite. The ACS onboard a satellite controls the actuators to orientate the satellite to its desired orientation such...
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| Format: | Thesis |
| Language: | English |
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2013
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| Online Access: | http://hdl.handle.net/10356/54760 |