A deep learning-based method for calculating aircraft wing loads

The purpose of this paper is to propose a novel aircraft wing loads calculation model, called long short-term memory residual network (LSTM-ResNet), which can evaluate the loads based on the strain distribution. To achieve this goal, firstly, the data acquisition experiment is designed and performed...

وصف كامل

التفاصيل البيبلوغرافية
الحاوية / القاعدة:Measurement + Control
المؤلفون الرئيسيون: Peiyao Wang, Mingxin Yu, Guang Yan, Jiabin Xia, Jiawei Liu, Lianqing Zhu
التنسيق: مقال
اللغة:الإنجليزية
منشور في: SAGE Publishing 2023-09-01
الوصول للمادة أونلاين:https://doi.org/10.1177/00202940221145971
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author Peiyao Wang
Mingxin Yu
Guang Yan
Jiabin Xia
Jiawei Liu
Lianqing Zhu
author_facet Peiyao Wang
Mingxin Yu
Guang Yan
Jiabin Xia
Jiawei Liu
Lianqing Zhu
author_sort Peiyao Wang
collection DOAJ
container_title Measurement + Control
description The purpose of this paper is to propose a novel aircraft wing loads calculation model, called long short-term memory residual network (LSTM-ResNet), which can evaluate the loads based on the strain distribution. To achieve this goal, firstly, the data acquisition experiment is designed and performed with a real aircraft wing. In this experiment, we used the Fiber Bragg Grating (FBG) technology as the measurement method to collect strain-load data from the aircraft wing. Then, we propose the LSTM-ResNet model with the one-dimensional convolutional(1D-CNN) architecture. This model is capable of extracting the temporal and spatial representational information from the strain-load data of the aircraft wing. Experimental results demonstrate that the proposed method effectively evaluate the loads of the aircraft wing. To prove the superiority of LSTM-ResNet model, we compared the proposed model with existing loads calculation methods on our experimental dataset. The results show it has a competitive average relative error (0.08%). Moreover, those promising results may pave the way to use the deep learning algorithm in aircraft wing loads calculation.
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spelling doaj-art-09c7cbc7ff3f413dbd4cd50d93ca48642025-08-19T21:50:04ZengSAGE PublishingMeasurement + Control0020-29402023-09-015610.1177/00202940221145971A deep learning-based method for calculating aircraft wing loadsPeiyao Wang0Mingxin Yu1Guang Yan2Jiabin Xia3Jiawei Liu4Lianqing Zhu5Key Laboratory of the Ministry of Education for Optoelectronic Measurement Technology and Instrument, Beijing Information Science & Technology University, Beijing, ChinaBeijing Laboratory of Biomedical Detection Technology and Instrument, Beijing, ChinaKey Laboratory of the Ministry of Education for Optoelectronic Measurement Technology and Instrument, Beijing Information Science & Technology University, Beijing, ChinaBeijing Laboratory of Biomedical Detection Technology and Instrument, Beijing, ChinaKey Laboratory of the Ministry of Education for Optoelectronic Measurement Technology and Instrument, Beijing Information Science & Technology University, Beijing, ChinaKey Laboratory of the Ministry of Education for Optoelectronic Measurement Technology and Instrument, Beijing Information Science & Technology University, Beijing, ChinaThe purpose of this paper is to propose a novel aircraft wing loads calculation model, called long short-term memory residual network (LSTM-ResNet), which can evaluate the loads based on the strain distribution. To achieve this goal, firstly, the data acquisition experiment is designed and performed with a real aircraft wing. In this experiment, we used the Fiber Bragg Grating (FBG) technology as the measurement method to collect strain-load data from the aircraft wing. Then, we propose the LSTM-ResNet model with the one-dimensional convolutional(1D-CNN) architecture. This model is capable of extracting the temporal and spatial representational information from the strain-load data of the aircraft wing. Experimental results demonstrate that the proposed method effectively evaluate the loads of the aircraft wing. To prove the superiority of LSTM-ResNet model, we compared the proposed model with existing loads calculation methods on our experimental dataset. The results show it has a competitive average relative error (0.08%). Moreover, those promising results may pave the way to use the deep learning algorithm in aircraft wing loads calculation.https://doi.org/10.1177/00202940221145971
spellingShingle Peiyao Wang
Mingxin Yu
Guang Yan
Jiabin Xia
Jiawei Liu
Lianqing Zhu
A deep learning-based method for calculating aircraft wing loads
title A deep learning-based method for calculating aircraft wing loads
title_full A deep learning-based method for calculating aircraft wing loads
title_fullStr A deep learning-based method for calculating aircraft wing loads
title_full_unstemmed A deep learning-based method for calculating aircraft wing loads
title_short A deep learning-based method for calculating aircraft wing loads
title_sort deep learning based method for calculating aircraft wing loads
url https://doi.org/10.1177/00202940221145971
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