Model Updating Strategy of the DLR-AIRMOD Test Structure

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dc.identifier.uri http://dx.doi.org/10.15488/2106
dc.identifier.uri http://www.repo.uni-hannover.de/handle/123456789/2131
dc.contributor.author Patelli, E.
dc.contributor.author Broggi, M.
dc.contributor.author Govers, Y.
dc.contributor.author Mottershead, J.E.
dc.date.accessioned 2017-10-24T08:25:13Z
dc.date.available 2017-10-24T08:25:13Z
dc.date.issued 2017
dc.identifier.citation Patelli, E.; Broggi, M.; Govers, Y.; Mottershead, J.E.: Model Updating Strategy of the DLR-AIRMOD Test Structure. In: Procedia Engineering 199 (2017), S. 978-983. DOI: https://doi.org/10.1016/j.proeng.2017.09.221
dc.description.abstract Considerable progresses have been made in computer-aided engineering for the high fidelity analysis of structures and systems. Traditionally, computer models are calibrated using deterministic procedures. However, different analysts produce different models based on different modelling approximations and assumptions. In addition, identically constructed structures and systems show different characteristic between each other. Hence, model updating needs to take account modelling and test-data variability. Stochastic model updating techniques such as sensitivity approach and Bayesian updating are now recognised as powerful approaches able to deal with unavoidable uncertainty and variability. This paper presents a high fidelity surrogate model that allows to significantly reduce the computational costs associated with the Bayesian model updating technique. A set of Artificial Neural Networks are proposed to replace multi non-linear input-output relationships of finite element (FE) models. An application for updating the model parameters of the FE model of the DRL-AIRMOD structure is presented. © 2017 The Authors. Published by Elsevier Ltd. eng
dc.language.iso eng
dc.publisher London : Elsevier Ltd.
dc.relation.ispartofseries Procedia Engineering 199 (2017)
dc.rights CC BY-NC-ND 4.0 Unported
dc.rights.uri https://creativecommons.org/licenses/by-nc-nd/4.0/
dc.subject Artificial Neural Networks eng
dc.subject Bayesian eng
dc.subject Model updating eng
dc.subject Simulation eng
dc.subject Bayesian networks eng
dc.subject Buckling eng
dc.subject Computer aided analysis eng
dc.subject Computer aided engineering eng
dc.subject Finite element method eng
dc.subject Neural networks eng
dc.subject Stochastic systems eng
dc.subject Structural dynamics eng
dc.subject Bayesian eng
dc.subject Bayesian model updating eng
dc.subject High fidelity analysis eng
dc.subject Model updating eng
dc.subject Sensitivity approach eng
dc.subject Simulation eng
dc.subject Stochastic model updating eng
dc.subject Uncertainty and variability eng
dc.subject Stochastic models eng
dc.subject.classification Konferenzschrift ger
dc.subject.ddc 600 | Technik ger
dc.title Model Updating Strategy of the DLR-AIRMOD Test Structure eng
dc.type Article
dc.type Text
dc.relation.issn 1877-7058
dc.relation.doi https://doi.org/10.1016/j.proeng.2017.09.221
dc.bibliographicCitation.volume 199
dc.bibliographicCitation.firstPage 978
dc.bibliographicCitation.lastPage 983
dc.description.version publishedVersion
tib.accessRights frei zug�nglich


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