Dynamic modelling and observation of micro-vibrations generated by a Single Gimbal Control Moment Gyro

Control Moment Gyros (CMGs) are commonly used as actuators of attitude control in spacecraft. Micro-vibrations generated by CMGs will influence the performance of high-sensitivity instruments on-board the spacecraft; however, the micro-vibration characteristics of CMGs are not yet clearly understood...

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Veröffentlicht in:	Journal of sound and vibration 2013-09, Vol.332 (19), p.4496-4516
Hauptverfasser:	Luo, Qing, Li, Dongxu, Zhou, Weiyong, Jiang, Jianping, Yang, Guang, Wei, Xinsheng
Format:	Artikel
Sprache:	eng
Schlagworte:	Dynamical systems Dynamics Gimbals Mathematical models Modelling Spacecraft Vibration
Online-Zugang:	Volltext
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