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Fuzzy finite element model updating of the DLR AIRMOD test structure
Applied Mathematical Modelling, Volume: 52, Pages: 512 - 526
Swansea University Authors: Johann Sienz , Michael Friswell, Sondipon Adhikari , Hamed Haddad Khodaparast
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DOI (Published version): 10.1016/j.apm.2017.08.001
Abstract
This article presents the application of finite-element fuzzy model updating to the DLR AIRMOD structure. The proposed approach is initially demonstrated on a simulated mass-spring system with three degrees of freedom. Considering the effect of the assembly process on variability measurements, modal...
Published in: | Applied Mathematical Modelling |
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ISSN: | 0307-904X |
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2017
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URI: | https://cronfa.swan.ac.uk/Record/cronfa34866 |
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2020-06-16T08:44:01.2482370 v2 34866 2017-08-04 Fuzzy finite element model updating of the DLR AIRMOD test structure 17bf1dd287bff2cb01b53d98ceb28a31 0000-0003-3136-5718 Johann Sienz Johann Sienz true false 5894777b8f9c6e64bde3568d68078d40 Michael Friswell Michael Friswell true false 4ea84d67c4e414f5ccbd7593a40f04d3 0000-0003-4181-3457 Sondipon Adhikari Sondipon Adhikari true false f207b17edda9c4c3ea074cbb7555efc1 0000-0002-3721-4980 Hamed Haddad Khodaparast Hamed Haddad Khodaparast true false 2017-08-04 This article presents the application of finite-element fuzzy model updating to the DLR AIRMOD structure. The proposed approach is initially demonstrated on a simulated mass-spring system with three degrees of freedom. Considering the effect of the assembly process on variability measurements, modal tests were carried out for the repeatedly disassembled and reassembled DLR AIRMOD structure. The histograms of the measured data attributed to the uncertainty of the structural components in terms of mass and stiffness are utilised to obtain the membership functions of the chosen fuzzy outputs and to determine the updated membership functions of the uncertain input parameters represented by fuzzy variables. In this regard, a fuzzy parameter is introduced to represent a set of interval parameters through the membership function, and a meta model (kriging, in this work) is used to speed up the updating. The use of non-probabilistic models, i.e. interval and fuzzy models, for updating models with uncertainties is often more practical when the large quantities of test data that are necessary for probabilistic model updating are unavailable. Journal Article Applied Mathematical Modelling 52 512 526 0307-904X Fuzzy variable; Model updating; AIRMOD structure 31 12 2017 2017-12-31 10.1016/j.apm.2017.08.001 COLLEGE NANME COLLEGE CODE Swansea University 2020-06-16T08:44:01.2482370 2017-08-04T08:45:25.2383367 Faculty of Science and Engineering School of Engineering and Applied Sciences - Uncategorised H. Haddad Khodaparast 1 Y. Govers 2 I. Dayyani 3 S. Adhikari 4 M. Link 5 M.I. Friswell 6 J.E. Mottershead 7 J. Sienz 8 Johann Sienz 0000-0003-3136-5718 9 Michael Friswell 10 Sondipon Adhikari 0000-0003-4181-3457 11 Hamed Haddad Khodaparast 0000-0002-3721-4980 12 0034866-21082017155123.pdf khodaparast2017v5.pdf 2017-08-21T15:51:23.5070000 Output 1278473 application/pdf Accepted Manuscript true 2018-08-12T00:00:00.0000000 true eng |
title |
Fuzzy finite element model updating of the DLR AIRMOD test structure |
spellingShingle |
Fuzzy finite element model updating of the DLR AIRMOD test structure Johann Sienz Michael Friswell Sondipon Adhikari Hamed Haddad Khodaparast |
title_short |
Fuzzy finite element model updating of the DLR AIRMOD test structure |
title_full |
Fuzzy finite element model updating of the DLR AIRMOD test structure |
title_fullStr |
Fuzzy finite element model updating of the DLR AIRMOD test structure |
title_full_unstemmed |
Fuzzy finite element model updating of the DLR AIRMOD test structure |
title_sort |
Fuzzy finite element model updating of the DLR AIRMOD test structure |
author_id_str_mv |
17bf1dd287bff2cb01b53d98ceb28a31 5894777b8f9c6e64bde3568d68078d40 4ea84d67c4e414f5ccbd7593a40f04d3 f207b17edda9c4c3ea074cbb7555efc1 |
author_id_fullname_str_mv |
17bf1dd287bff2cb01b53d98ceb28a31_***_Johann Sienz 5894777b8f9c6e64bde3568d68078d40_***_Michael Friswell 4ea84d67c4e414f5ccbd7593a40f04d3_***_Sondipon Adhikari f207b17edda9c4c3ea074cbb7555efc1_***_Hamed Haddad Khodaparast |
author |
Johann Sienz Michael Friswell Sondipon Adhikari Hamed Haddad Khodaparast |
author2 |
H. Haddad Khodaparast Y. Govers I. Dayyani S. Adhikari M. Link M.I. Friswell J.E. Mottershead J. Sienz Johann Sienz Michael Friswell Sondipon Adhikari Hamed Haddad Khodaparast |
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Applied Mathematical Modelling |
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10.1016/j.apm.2017.08.001 |
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description |
This article presents the application of finite-element fuzzy model updating to the DLR AIRMOD structure. The proposed approach is initially demonstrated on a simulated mass-spring system with three degrees of freedom. Considering the effect of the assembly process on variability measurements, modal tests were carried out for the repeatedly disassembled and reassembled DLR AIRMOD structure. The histograms of the measured data attributed to the uncertainty of the structural components in terms of mass and stiffness are utilised to obtain the membership functions of the chosen fuzzy outputs and to determine the updated membership functions of the uncertain input parameters represented by fuzzy variables. In this regard, a fuzzy parameter is introduced to represent a set of interval parameters through the membership function, and a meta model (kriging, in this work) is used to speed up the updating. The use of non-probabilistic models, i.e. interval and fuzzy models, for updating models with uncertainties is often more practical when the large quantities of test data that are necessary for probabilistic model updating are unavailable. |
published_date |
2017-12-31T07:08:55Z |
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11.047306 |