In order to solve the problems of large number of conditions at inherent frequencies and low prediction accuracy when using multiple multivariate linear regression methods for vibration response prediction alone, an elastic-net regularization method is proposed. Firstly, a multi-input and multioutput linear regression model of the multipoint frequency domain vibration response is trained using historical data at each frequency point. Secondly, the trained model under each frequency point is improved by the elastic regularization. Finally, the model is used in a working situation. The predicted vibration response on the experimental dataset of cylindrical shell acoustic vibration showed that the improvement of the multivariate regression vib...
The parametric approach to eliminating the temperature-caused modal variability in vibration-based s...
This study aims to correlate the vibration data with quantitative indicators of structural health by...
International audienceA critical step in aircraft design is to specify the vibration levels that onb...
Abstract: Because frequency load identification method will confront with the ill-posed problem of f...
An identification algorithm for vibrating dynamic characterization by using artificial neural networ...
AbstractAircraft vibration response environment prediction, which is adopted in aircraft initial veh...
Inspired by deep learning applications in structural mechanics, we focus on how to train two predict...
A method of predicting broadband random vibration criteria for components on space vehicles is prese...
This study is designed to develop an acceleration response spectrum that can be used in vibration se...
International audienceVibration levels that onboard equipment must be able to withstand throughout t...
Abstract Practical engineering prediction models for flow-induced vibration are needed in the desig...
This study develops a high performance grading process based on the analysis of acoustic vibrations ...
Site response spectrum is one of the key factors to determine the maximum acceleration and displacem...
Site response spectrum is one of the key factors to determine the maximum acceleration and displacem...
International audienceDynamic forces reconstruction from vibration data is an ill-posed inverse prob...
The parametric approach to eliminating the temperature-caused modal variability in vibration-based s...
This study aims to correlate the vibration data with quantitative indicators of structural health by...
International audienceA critical step in aircraft design is to specify the vibration levels that onb...
Abstract: Because frequency load identification method will confront with the ill-posed problem of f...
An identification algorithm for vibrating dynamic characterization by using artificial neural networ...
AbstractAircraft vibration response environment prediction, which is adopted in aircraft initial veh...
Inspired by deep learning applications in structural mechanics, we focus on how to train two predict...
A method of predicting broadband random vibration criteria for components on space vehicles is prese...
This study is designed to develop an acceleration response spectrum that can be used in vibration se...
International audienceVibration levels that onboard equipment must be able to withstand throughout t...
Abstract Practical engineering prediction models for flow-induced vibration are needed in the desig...
This study develops a high performance grading process based on the analysis of acoustic vibrations ...
Site response spectrum is one of the key factors to determine the maximum acceleration and displacem...
Site response spectrum is one of the key factors to determine the maximum acceleration and displacem...
International audienceDynamic forces reconstruction from vibration data is an ill-posed inverse prob...
The parametric approach to eliminating the temperature-caused modal variability in vibration-based s...
This study aims to correlate the vibration data with quantitative indicators of structural health by...
International audienceA critical step in aircraft design is to specify the vibration levels that onb...