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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Główni autorzy:	GUO Yanning, DENG Yuchen, RAN Guangtao, LIU Fucheng
Format:	Artigo
Język:	Inglês
Wydane:	Editorial Office of Transactions of Nanjing University of Aeronautics and Astronautics 2025-12-01
Seria:	Transactions of Nanjing University of Aeronautics and Astronautics
Hasła przedmiotowe:	large space structure （lss） flexible spacecraft control optimal placement of actuator vibration control rigid-flexible coupling spacecraft
Dostęp online:	https://tnuaa.nuaa.edu.cn/njhkhten/article/html/202506001?st=article_issue
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