Coupling‑Reduced Optimal Placement of Piezoelectric Actuators for Spacecraft with Flexible Telescope

The oscillation of large space structure （LSS） can be easily induced because of its low vibration frequency. The coupling effect between LSS vibration control and attitude control can significantly reduce the overall performance of the control system， especially when the scale of flexible structure...

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Λεπτομέρειες βιβλιογραφικής εγγραφής

Κύριοι συγγραφείς:	GUO Yanning, DENG Yuchen, RAN Guangtao, LIU Fucheng
Μορφή:	Artigo
Γλώσσα:	Inglês
Έκδοση:	Editorial Office of Transactions of Nanjing University of Aeronautics and Astronautics 2025-12-01
Σειρά:	Transactions of Nanjing University of Aeronautics and Astronautics
Θέματα:	large space structure （lss） flexible spacecraft control optimal placement of actuator vibration control rigid-flexible coupling spacecraft
Διαθέσιμο Online:	https://tnuaa.nuaa.edu.cn/njhkhten/article/html/202506001?st=article_issue
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