Anti-Disturbance Gimbal Control via Adaptive Proportional-Integral-Resonant Controller and ESO for Control Moment Gyroscope with Vibration Isolator
In order to mitigate the effects of micro-vibrations due to control moment gyroscopes (CMGs) on spacecraft attitude control system, they are often mounted on isolation platforms. However, the flexible deformation of isolators may cause certain disturbances in CMG gimbal servo systems. In addition, g...
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| Autori principali: | , , |
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| Natura: | Artigo |
| Lingua: | Inglês |
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MDPI AG
2026-04-01
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| Serie: | Actuators |
| Soggetti: | |
| Accesso online: | https://www.mdpi.com/2076-0825/15/4/215 |
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