Active vibration control of a slewing spacecraft's panel using H infinity control

作者：Khushnood, Muhammad Atif^*; Wang, Xiaogang; Cui, Naigang

来源：Journal of Vibroengineering, 2016, 18(5): 2959-2973.

DOI：10.21595/jve.2016.16887

• active vibration control
• slewing spacecraft
• H infinity control

Application of H infinity control for multimodal vibration suppression of a slewing spacecraft using piezoelectric actuators is presented in this paper. For treating vibration suppression independent of attitude control law while taking into account relative modal responses; a method for modeling effect of attitude maneuver excitations as modal disturbances is proposed. Commercial finite element software ANSYS is used for obtaining system model. Modifications of system model and selection of weights required for control synthesis are explained in detail. The method is applied for suppressing vibration of first two modes of a flexible spacecraft. Results showed effectiveness of the proposed method.

• 出版日期2016-8
• 单位哈尔滨工业大学