Vibration Suppression of a Maneuvering Flexible Spacecraft with Actuator Dynamic
This paper presents a study concerning active vibration control of a smart, flexible spacecraft during attitude maneuver using thrusters/ a reaction wheel and piezoelectric patches. The large-angle maneuver and residual vibration of the spacecraft are controlled utilizing an extended Lyapunov-based...
Kaydedildi:
| Asıl Yazarlar: | , |
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| Materyal Türü: | Artigo |
| Dil: | Persa |
| Baskı/Yayın Bilgisi: |
Aerospace Research Institute (ARI)
2021-05-01
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| Seri Bilgileri: | فناوری در مهندسی هوافضا |
| Konular: | |
| Online Erişim: | https://jtae.ari.ac.ir/article_129873_4e42579b75216fecf458e62e1564ae2c.pdf |
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