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FOSS-Based Method for Thin-Walled Structure Deformation Perception and Shape Reconstruction
To improve the accuracy of deformation perception and shape reconstruction of flexible thin-walled structures, this paper proposes a method based on the combination of FOSS (fiber optic sensor system) and machine learning. In this method, the sample collection of strain measurement and deformation c...
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Published in: | Micromachines (Basel) 2023-03, Vol.14 (4), p.794 |
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description | To improve the accuracy of deformation perception and shape reconstruction of flexible thin-walled structures, this paper proposes a method based on the combination of FOSS (fiber optic sensor system) and machine learning. In this method, the sample collection of strain measurement and deformation change at each measuring point of the flexible thin-walled structure was completed by ANSYS finite element analysis. The outliers were removed by the OCSVM (one-class support vector machine) model, and the unique mapping relationship between the strain value and the deformation variables (three directions of x-, y-, and z-axis) at each point was completed by a neural-network model. The test results show that the maximum error of the measuring point in the direction of the three coordinate axes: the x-axis is 2.01%, the y-axis is 29.49%, and the z-axis is 15.52%. The error of the coordinates in the y and z directions was large, and the deformation variables were small, the reconstructed shape had good consistency with the deformation state of the specimen under the existing test environment. This method provides a new idea with high accuracy for real-time monitoring and shape reconstruction of flexible thin-walled structures such as wings, helicopter blades, and solar panels. |
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In this method, the sample collection of strain measurement and deformation change at each measuring point of the flexible thin-walled structure was completed by ANSYS finite element analysis. The outliers were removed by the OCSVM (one-class support vector machine) model, and the unique mapping relationship between the strain value and the deformation variables (three directions of x-, y-, and z-axis) at each point was completed by a neural-network model. The test results show that the maximum error of the measuring point in the direction of the three coordinate axes: the x-axis is 2.01%, the y-axis is 29.49%, and the z-axis is 15.52%. The error of the coordinates in the y and z directions was large, and the deformation variables were small, the reconstructed shape had good consistency with the deformation state of the specimen under the existing test environment. This method provides a new idea with high accuracy for real-time monitoring and shape reconstruction of flexible thin-walled structures such as wings, helicopter blades, and solar panels.</description><identifier>ISSN: 2072-666X</identifier><identifier>EISSN: 2072-666X</identifier><identifier>DOI: 10.3390/mi14040794</identifier><identifier>PMID: 37421029</identifier><language>eng</language><publisher>Switzerland: MDPI AG</publisher><subject>Accuracy ; Aircraft ; Algorithms ; Analysis ; BP neural network ; Data analysis ; Deformation ; Equipment and supplies ; Error analysis ; Fiber optics ; fiber-optic sensor system ; Finite element method ; Helicopters ; Machine learning ; Methods ; Model testing ; Neural networks ; one-class SVM ; Outliers (statistics) ; Perception ; Reconstruction ; Sensors ; shape reconfiguration ; Simulation ; Strain measurement ; Support vector machines ; Thin wall structures</subject><ispartof>Micromachines (Basel), 2023-03, Vol.14 (4), p.794</ispartof><rights>COPYRIGHT 2023 MDPI AG</rights><rights>2023 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><rights>2023 by the authors. 2023</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c471t-cba2de6b173b0aea27f39800ee9f3aad890b3c7bb3aa65eebe353b65a2e0dae83</cites><orcidid>0000-0002-1356-0969</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.proquest.com/docview/2806584011/fulltextPDF?pq-origsite=primo$$EPDF$$P50$$Gproquest$$Hfree_for_read</linktopdf><linktohtml>$$Uhttps://www.proquest.com/docview/2806584011?pq-origsite=primo$$EHTML$$P50$$Gproquest$$Hfree_for_read</linktohtml><link.rule.ids>230,314,727,780,784,885,25753,27924,27925,37012,37013,44590,53791,53793,74998</link.rule.ids><backlink>$$Uhttps://www.ncbi.nlm.nih.gov/pubmed/37421029$$D View this record in MEDLINE/PubMed$$Hfree_for_read</backlink></links><search><creatorcontrib>Wu, Huifeng</creatorcontrib><creatorcontrib>Dong, Rui</creatorcontrib><creatorcontrib>Xu, Qiwei</creatorcontrib><creatorcontrib>Liu, Zheng</creatorcontrib><creatorcontrib>Liang, Lei</creatorcontrib><title>FOSS-Based Method for Thin-Walled Structure Deformation Perception and Shape Reconstruction</title><title>Micromachines (Basel)</title><addtitle>Micromachines (Basel)</addtitle><description>To improve the accuracy of deformation perception and shape reconstruction of flexible thin-walled structures, this paper proposes a method based on the combination of FOSS (fiber optic sensor system) and machine learning. In this method, the sample collection of strain measurement and deformation change at each measuring point of the flexible thin-walled structure was completed by ANSYS finite element analysis. The outliers were removed by the OCSVM (one-class support vector machine) model, and the unique mapping relationship between the strain value and the deformation variables (three directions of x-, y-, and z-axis) at each point was completed by a neural-network model. The test results show that the maximum error of the measuring point in the direction of the three coordinate axes: the x-axis is 2.01%, the y-axis is 29.49%, and the z-axis is 15.52%. The error of the coordinates in the y and z directions was large, and the deformation variables were small, the reconstructed shape had good consistency with the deformation state of the specimen under the existing test environment. This method provides a new idea with high accuracy for real-time monitoring and shape reconstruction of flexible thin-walled structures such as wings, helicopter blades, and solar panels.</description><subject>Accuracy</subject><subject>Aircraft</subject><subject>Algorithms</subject><subject>Analysis</subject><subject>BP neural network</subject><subject>Data analysis</subject><subject>Deformation</subject><subject>Equipment and supplies</subject><subject>Error analysis</subject><subject>Fiber optics</subject><subject>fiber-optic sensor system</subject><subject>Finite element method</subject><subject>Helicopters</subject><subject>Machine learning</subject><subject>Methods</subject><subject>Model testing</subject><subject>Neural networks</subject><subject>one-class SVM</subject><subject>Outliers (statistics)</subject><subject>Perception</subject><subject>Reconstruction</subject><subject>Sensors</subject><subject>shape reconfiguration</subject><subject>Simulation</subject><subject>Strain measurement</subject><subject>Support vector machines</subject><subject>Thin wall structures</subject><issn>2072-666X</issn><issn>2072-666X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><sourceid>PIMPY</sourceid><sourceid>DOA</sourceid><recordid>eNpdkt9rFDEQxxdRbKl98Q-QBV9E2Jpfu9k8SVutFioVr6LgQ5gks3c5djdnsiv435u7q7U1gWQy85nvJGGK4jklJ5wr8mbwVBBBpBKPikNGJKuapvn--J59UByntCZ5SKny8rQ44FIwSpg6LH5cXC8W1RkkdOUnnFbBlV2I5c3Kj9U36PvsXkxxttMcsXyHOTbA5MNYfsZocbMzYczQCjZYfkEbxrTjc-BZ8aSDPuHx7X5UfL14f3P-sbq6_nB5fnpVWSHpVFkDzGFjqOSGAAKTHVctIYiq4wCuVcRwK43Jh6ZGNMhrbpoaGBIH2PKj4nKv6wKs9Sb6AeJvHcDrnSPEpYY4edujlm3dqq6tnRCNICiBQe0cMpIrqtq4rPV2r7WZzYDO4jhF6B-IPoyMfqWX4ZemhIpGSZUVXt0qxPBzxjTpwSeLfQ8jhjlp1vKaSUrEFn35H7oOcxzzX2WKNHUrCKWZOtlTS8gv8GMXcmGbp8PB5__Gzmf_qRRSNDWX24TX-wQbQ0oRu7vrU6K3TaP_NU2GX9x_8B36t0X4H-fmvOU</recordid><startdate>20230331</startdate><enddate>20230331</enddate><creator>Wu, Huifeng</creator><creator>Dong, Rui</creator><creator>Xu, Qiwei</creator><creator>Liu, Zheng</creator><creator>Liang, Lei</creator><general>MDPI AG</general><general>MDPI</general><scope>NPM</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>FR3</scope><scope>HCIFZ</scope><scope>L6V</scope><scope>L7M</scope><scope>M7S</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope><scope>7X8</scope><scope>5PM</scope><scope>DOA</scope><orcidid>https://orcid.org/0000-0002-1356-0969</orcidid></search><sort><creationdate>20230331</creationdate><title>FOSS-Based Method for Thin-Walled Structure Deformation Perception and Shape Reconstruction</title><author>Wu, Huifeng ; Dong, Rui ; Xu, Qiwei ; Liu, Zheng ; Liang, Lei</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c471t-cba2de6b173b0aea27f39800ee9f3aad890b3c7bb3aa65eebe353b65a2e0dae83</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Accuracy</topic><topic>Aircraft</topic><topic>Algorithms</topic><topic>Analysis</topic><topic>BP neural network</topic><topic>Data analysis</topic><topic>Deformation</topic><topic>Equipment and supplies</topic><topic>Error analysis</topic><topic>Fiber optics</topic><topic>fiber-optic sensor system</topic><topic>Finite element method</topic><topic>Helicopters</topic><topic>Machine learning</topic><topic>Methods</topic><topic>Model testing</topic><topic>Neural networks</topic><topic>one-class SVM</topic><topic>Outliers (statistics)</topic><topic>Perception</topic><topic>Reconstruction</topic><topic>Sensors</topic><topic>shape reconfiguration</topic><topic>Simulation</topic><topic>Strain measurement</topic><topic>Support vector machines</topic><topic>Thin wall structures</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Wu, Huifeng</creatorcontrib><creatorcontrib>Dong, Rui</creatorcontrib><creatorcontrib>Xu, Qiwei</creatorcontrib><creatorcontrib>Liu, Zheng</creatorcontrib><creatorcontrib>Liang, Lei</creatorcontrib><collection>PubMed</collection><collection>CrossRef</collection><collection>Electronics & Communications Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni)</collection><collection>ProQuest Central</collection><collection>ProQuest Central Essentials</collection><collection>AUTh Library subscriptions: ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central</collection><collection>Engineering Research Database</collection><collection>SciTech Premium Collection (Proquest) (PQ_SDU_P3)</collection><collection>ProQuest Engineering Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Engineering Database</collection><collection>Publicly Available Content Database (Proquest) (PQ_SDU_P3)</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Engineering Collection</collection><collection>MEDLINE - Academic</collection><collection>PubMed Central (Full Participant titles)</collection><collection>DOAJÂ Directory of Open Access Journals</collection><jtitle>Micromachines (Basel)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Wu, Huifeng</au><au>Dong, Rui</au><au>Xu, Qiwei</au><au>Liu, Zheng</au><au>Liang, Lei</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>FOSS-Based Method for Thin-Walled Structure Deformation Perception and Shape Reconstruction</atitle><jtitle>Micromachines (Basel)</jtitle><addtitle>Micromachines (Basel)</addtitle><date>2023-03-31</date><risdate>2023</risdate><volume>14</volume><issue>4</issue><spage>794</spage><pages>794-</pages><issn>2072-666X</issn><eissn>2072-666X</eissn><abstract>To improve the accuracy of deformation perception and shape reconstruction of flexible thin-walled structures, this paper proposes a method based on the combination of FOSS (fiber optic sensor system) and machine learning. In this method, the sample collection of strain measurement and deformation change at each measuring point of the flexible thin-walled structure was completed by ANSYS finite element analysis. The outliers were removed by the OCSVM (one-class support vector machine) model, and the unique mapping relationship between the strain value and the deformation variables (three directions of x-, y-, and z-axis) at each point was completed by a neural-network model. The test results show that the maximum error of the measuring point in the direction of the three coordinate axes: the x-axis is 2.01%, the y-axis is 29.49%, and the z-axis is 15.52%. The error of the coordinates in the y and z directions was large, and the deformation variables were small, the reconstructed shape had good consistency with the deformation state of the specimen under the existing test environment. This method provides a new idea with high accuracy for real-time monitoring and shape reconstruction of flexible thin-walled structures such as wings, helicopter blades, and solar panels.</abstract><cop>Switzerland</cop><pub>MDPI AG</pub><pmid>37421029</pmid><doi>10.3390/mi14040794</doi><orcidid>https://orcid.org/0000-0002-1356-0969</orcidid><oa>free_for_read</oa></addata></record> |
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subjects | Accuracy Aircraft Algorithms Analysis BP neural network Data analysis Deformation Equipment and supplies Error analysis Fiber optics fiber-optic sensor system Finite element method Helicopters Machine learning Methods Model testing Neural networks one-class SVM Outliers (statistics) Perception Reconstruction Sensors shape reconfiguration Simulation Strain measurement Support vector machines Thin wall structures |
title | FOSS-Based Method for Thin-Walled Structure Deformation Perception and Shape Reconstruction |
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