Testing & performance characterization of a CubeSat attitude control system
This paper describes the design, testing & performance characterization of a Reaction Wheel-based attitude Control System for the SCOOB-I Nanosatellite. A reaction wheel is simply a variant of a flywheel that is primarily used in satellites for attitude control and is usually used when the satel...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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Nanyang Technological University
2020
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| Online Access: | https://hdl.handle.net/10356/140642 |