Optimal Sensor Placement Based on Eigenvalues Analysis for Sensing Deformation of Wing Frame Using iFEM
For real time monitoring of the wing state, in this paper, the inverse Finite Element Method (iFEM) is applied, which describes the displacement field of beam according to the Timoshenko theory, to sense the wing frame deformation. In order to maintain the accuracy and stability of frame deformation...
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doaj-c76e452615bd49fd8b13109da501f4332020-11-25T00:34:38ZengMDPI AGSensors1424-82202018-07-01188242410.3390/s18082424s18082424Optimal Sensor Placement Based on Eigenvalues Analysis for Sensing Deformation of Wing Frame Using iFEMYong Zhao0Jingli Du1Hong Bao2Qian Xu3Key Laboratory of Electronic Equipment Structure Design of Ministry of Education, Xidian University, Xi’an 710071, ChinaKey Laboratory of Electronic Equipment Structure Design of Ministry of Education, Xidian University, Xi’an 710071, ChinaKey Laboratory of Electronic Equipment Structure Design of Ministry of Education, Xidian University, Xi’an 710071, ChinaXinjiang Observatory, National Astronomical Observatories, Chinese Academy of Sciences, Urumqi 830011, ChinaFor real time monitoring of the wing state, in this paper, the inverse Finite Element Method (iFEM) is applied, which describes the displacement field of beam according to the Timoshenko theory, to sense the wing frame deformation. In order to maintain the accuracy and stability of frame deformation sensing with iFEM, an optimal placement model of strain sensors based on eigenvalue analysis is constructed. Through the model solution with the Particle Swarm Optimization (PSO) algorithm, two different optimal placement schemes of sensors are obtained. Finally, a simulation is performed on a simple cantilever beam and a static load experiment is conducted on an aluminum alloy wing frame. The results demonstrate that the iFEM is able to accurately sense the deformation of the wing frame, when the two optimal placement schemes of sensors are used.http://www.mdpi.com/1424-8220/18/8/2424deformation sensinginverse Finite Element MethodTimoshenko beam theoryoptimal placement of sensorseigenvalue analysis |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Yong Zhao Jingli Du Hong Bao Qian Xu |
spellingShingle |
Yong Zhao Jingli Du Hong Bao Qian Xu Optimal Sensor Placement Based on Eigenvalues Analysis for Sensing Deformation of Wing Frame Using iFEM Sensors deformation sensing inverse Finite Element Method Timoshenko beam theory optimal placement of sensors eigenvalue analysis |
author_facet |
Yong Zhao Jingli Du Hong Bao Qian Xu |
author_sort |
Yong Zhao |
title |
Optimal Sensor Placement Based on Eigenvalues Analysis for Sensing Deformation of Wing Frame Using iFEM |
title_short |
Optimal Sensor Placement Based on Eigenvalues Analysis for Sensing Deformation of Wing Frame Using iFEM |
title_full |
Optimal Sensor Placement Based on Eigenvalues Analysis for Sensing Deformation of Wing Frame Using iFEM |
title_fullStr |
Optimal Sensor Placement Based on Eigenvalues Analysis for Sensing Deformation of Wing Frame Using iFEM |
title_full_unstemmed |
Optimal Sensor Placement Based on Eigenvalues Analysis for Sensing Deformation of Wing Frame Using iFEM |
title_sort |
optimal sensor placement based on eigenvalues analysis for sensing deformation of wing frame using ifem |
publisher |
MDPI AG |
series |
Sensors |
issn |
1424-8220 |
publishDate |
2018-07-01 |
description |
For real time monitoring of the wing state, in this paper, the inverse Finite Element Method (iFEM) is applied, which describes the displacement field of beam according to the Timoshenko theory, to sense the wing frame deformation. In order to maintain the accuracy and stability of frame deformation sensing with iFEM, an optimal placement model of strain sensors based on eigenvalue analysis is constructed. Through the model solution with the Particle Swarm Optimization (PSO) algorithm, two different optimal placement schemes of sensors are obtained. Finally, a simulation is performed on a simple cantilever beam and a static load experiment is conducted on an aluminum alloy wing frame. The results demonstrate that the iFEM is able to accurately sense the deformation of the wing frame, when the two optimal placement schemes of sensors are used. |
topic |
deformation sensing inverse Finite Element Method Timoshenko beam theory optimal placement of sensors eigenvalue analysis |
url |
http://www.mdpi.com/1424-8220/18/8/2424 |
work_keys_str_mv |
AT yongzhao optimalsensorplacementbasedoneigenvaluesanalysisforsensingdeformationofwingframeusingifem AT jinglidu optimalsensorplacementbasedoneigenvaluesanalysisforsensingdeformationofwingframeusingifem AT hongbao optimalsensorplacementbasedoneigenvaluesanalysisforsensingdeformationofwingframeusingifem AT qianxu optimalsensorplacementbasedoneigenvaluesanalysisforsensingdeformationofwingframeusingifem |
_version_ |
1725312388422434816 |