Active vibration control of a slewing spacecraft’s panel using H∞ control

Application of H∞ 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...

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Bibliographic Details
Main Authors: Muhammad Atif Khushnood, Xiaogang Wang, Naigang Cui
Format: Article
Language:English
Published: JVE International 2016-08-01
Series:Journal of Vibroengineering
Subjects:
Online Access:https://www.jvejournals.com/article/16887