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