Active Control of Vibration


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Sun, J. Sound Vib. CrossRef Google Scholar. Balas, M. Guidance and Control 2 , , — Benhabib, R. Guidance and Control 4 , , — MathSciNet Google Scholar. Gawronski, W.

Demo of Bosch Active Vibration Control

Karnopp, D. Mechanical Design , , — Elliott, S.

Active Vibration Control Platform uses feedback to control vibrations - Series

Frampton, K. Chou, K. IEEE Conf. Aubrun, J. Guidance and Control 3 , , — Ungar, E.


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Beranck and I. Ver eds , Wiley, Chichester, , Chapter Vibration and Acoustics , , — Serrand, M.

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Skogestad, S. Kim, S-M. Huang, X. Pickles, J.

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Le Henaff, B. The vibration loads of a helicopter rotor are transmitted to the fuselage through gearbox support struts and cause severe vibration of the fuselage. A piezoelectric stack actuator has the advantages of light weight, a large driving force, small driving displacement, a wide working frequency range, and a fast response speed; it is an ideal actuator for the active vibration control of structures.

The piezoelectric stack actuators are installed on the gearbox support struts, which can effectively control the vibration of the helicopter fuselage. Google Scholar.

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Volume 56, Issue 2. No Access Full-Length Papers.

Candidate, College of Aerospace Engineering. Tools Add to favorites Download citation Track citations.

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