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Closed loop vibration control experiments on a rotor with blade mounted actuation
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Atlanta, GA
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Prechtl, E.F.1
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Design and testing of a double X-frame piezoelectric actuator
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Newport Beach, CA
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Helicopter vibration reduction through cyclic variations in rotor blade root stiffness
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An actively tunable vibration absorber designed to control aeroelastic response
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Norfolk, VA
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Aeroelastic analysis of a helicopter rotor blade with active impedance control at the root
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Feed-forward piezoelectric structural control: An application to aircraft cabin noise reduction
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A. Grewal, D. G. Zimcik, and B. Leigh "Feed-forward Piezoelectric Structural Control: An Application to Aircraft Cabin Noise Reduction," Journal of Aircraft, 38(1), 164-173, 2001.
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Active control of multi-tonal noise with reference generator based on on-line frequency estimation
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