Testing & performance characterization of a CubeSat attitude control system

• المؤلف الرئيسي: Tan, Yong Kai
• مؤلفون آخرون: Amal Chandran
• التنسيق: Final Year Project
• اللغة: English
• منشور في: Nanyang Technological University 2020
• الموضوعات: Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/140642
• المؤسسة: Nanyang Technological University

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...