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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2009, Vol. 30 ›› Issue (11): 2087-2092.

• 固体力学与飞行器设计 • Previous Articles     Next Articles

LS-SVMbased Method for Modal Parameter Identification

Fu Zhichao1, Cheng Wei1, Xu Cheng2   

  1. 1School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics 2North China Power Engineering (Beijing) Co. Ltd.
  • Received:2008-09-25 Revised:2008-12-03 Online:2009-11-25 Published:2009-11-25
  • Contact: Fu Zhichao

Abstract: A leastsquares support vector regression (LSSVR) technique is applied to modal parameter identification in this article. While the present least squares support vector machines (LSSVM) exhibit two natural drawbacks of insufficient robustness and sparseness, a novel algorithm that can overcome these drawbacks is proposed. An LSSVMbased method employing the auto regression moving average (ARMA) time series is presented for linear structural parameter identification using the observed vibration data. Both numerical evaluation and experimental validation demonstrate that the LSSVMbased method identifies structural modal parameters accurately and quickly.

Key words: least squares support vector machines (LSSVM), ARMA model, robustness, sparseness, modal analysis

CLC Number: