In this paper an approach for the identification of the modal properties of a time-varying system in the Operational Modal Analysis (OMA) framework is presented. The natural frequencies are estimated using the Hilbert-Huang Transform Method (HHTM) for its capabilities to track the time variations of such modal properties. Then, the Hilbert Transform Method (HTM) is applied for estimating both the damping ratios and mode shapes, not available from the previous method. The developed approach has been numerically assessed considering an aeroelastic system. The accuracy in time-tracking the modal parameters has been investigated by analyzing the numerically simulated time responses from a panel flutter model subjected to random operating loading for which the analytical solution is available.
Modal parameter estimate of time-varying system using operational modal analysis based on hilbert transform / Conti, Elisabetta; Saltari, Francesco; Eugeni, Marco; Camerini, Valerio; Coppotelli, Giuliano. - 1:(2017), pp. 489-502. (Intervento presentato al convegno 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017 tenutosi a Como, Italy).
Modal parameter estimate of time-varying system using operational modal analysis based on hilbert transform
Conti, ElisabettaMembro del Collaboration Group
;Saltari, FrancescoMembro del Collaboration Group
;Eugeni, MarcoMembro del Collaboration Group
;Camerini, ValerioMembro del Collaboration Group
;Coppotelli, Giuliano
Membro del Collaboration Group
2017
Abstract
In this paper an approach for the identification of the modal properties of a time-varying system in the Operational Modal Analysis (OMA) framework is presented. The natural frequencies are estimated using the Hilbert-Huang Transform Method (HHTM) for its capabilities to track the time variations of such modal properties. Then, the Hilbert Transform Method (HTM) is applied for estimating both the damping ratios and mode shapes, not available from the previous method. The developed approach has been numerically assessed considering an aeroelastic system. The accuracy in time-tracking the modal parameters has been investigated by analyzing the numerically simulated time responses from a panel flutter model subjected to random operating loading for which the analytical solution is available.File | Dimensione | Formato | |
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