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Experimental Demonstration of H[unknown] Control based Active Vibration Suppression in Composite Fin-tip of Aircraft using Optimally Placed Piezoelectric Patch Actuators
Experimental Demonstration of H[unknown] Control based Active Vibration Suppression in Composite Fin-tip of Aircraft using Optimally Placed Piezoelectric Patch Actuators
Experimental Demonstration of H[unknown] Control based Active Vibration Suppression in Composite Fin-tip of Aircraft using Optimally Placed Piezoelectric Patch Actuators
Rao, A.K. (author) / Natesan, K. (author) / Bhat, M.S. (author) / Ganguli, R. (author)
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES ; 19 ; 651-669
2008-01-01
19 pages
Article (Journal)
English
DDC:
620.11
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