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: | , , |
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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 |