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