Power System Design, Analysis, and Power Electronics Implementation on Generic Nanosatellite Bus (GNB) Spacecraft
The development of a multi-mission small spacecraft power system is described. This system has been designed for the University of Toronto Space Flight Laboratory Generic Nanosatellite Bus (GNB), an approximately 20cm cubical spacecraft with no deployed solar arrays. The GNB is inherently power-gene...
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| Language: | en_ca |
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2009
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| Online Access: | http://hdl.handle.net/1807/18940 |