Parameter Tuning Of An Active Force Control For Cmg-Based Controlled Small Satellite

A control moment gyroscope (CMG) system is the most appropriate actuator to be actualized in attitude determination and control system (ADCS) of small satellite. These actuators can provide unique torque, angular momentum and slew rate capabilities to small satellites without any increase in power,...

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Bibliographic Details
Main Author: Linghan, Samanaseh
Format: Monograph
Language:English
Published: Universiti Sains Malaysia 2019
Subjects:
Online Access:http://eprints.usm.my/58685/1/Parameter%20Tuning%20Of%20An%20Active%20Force%20Control%20For%20Cmg-Based%20Controlled%20Small%20Satellite.pdf
http://eprints.usm.my/58685/
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