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MIMO Multi-Frequency Active Vibration Control for Aircraft Panel Structure Using Piezoelectric Actuators

Author(s): (School of Aeronautics, Northwestern Polytechnical University, Xi’an, Shaanxi 710072, P. R. China)
(School of Aeronautics, Northwestern Polytechnical University, Xi’an, Shaanxi 710072, P. R. China)
(School of Aeronautics, Northwestern Polytechnical University, Xi’an, Shaanxi 710072, P. R. China)
(School of Aeronautics, Northwestern Polytechnical University, Xi’an, Shaanxi 710072, P. R. China)
Medium: journal article
Language(s): English
Published in: International Journal of Structural Stability and Dynamics, , n. 14, v. 23
DOI: 10.1142/s0219455423501572
Structurae cannot make the full text of this publication available at this time. The full text can be accessed through the publisher via the DOI: 10.1142/s0219455423501572.
  • About this
    data sheet
  • Reference-ID
    10713327
  • Published on:
    21/03/2023
  • Last updated on:
    01/09/2023
 
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