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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Bibliographic Details
Main Author: Tan, Yong Kai
Other Authors: Amal Chandran
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2020
Subjects:
Online Access:https://hdl.handle.net/10356/140642
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Institution: Nanyang Technological University
Language: English

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