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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. (Autor:in) / Natesan, K. (Autor:in) / Bhat, M.S. (Autor:in) / Ganguli, R. (Autor:in)
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES ; 19 ; 651-669
01.01.2008
19 pages
Aufsatz (Zeitschrift)
Englisch
DDC:
620.11
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