Attitude Determination and Control Hardware Development for Small Satellites
The development of a small spacecraft attitude determination and control subsystem is described. This subsystem is part of The Space Flight Laboratory's Generic Nanosatellite Bus. With a 20cm3 body, the bus has an attitude determination and control subsystem capable of full three-axis stabili...
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| Language: | en_ca |
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2011
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| Online Access: | http://hdl.handle.net/1807/29545 |