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...
| الحاوية / القاعدة: | Measurement + Control |
|---|---|
| المؤلفون الرئيسيون: | , , , , , |
| التنسيق: | مقال |
| اللغة: | الإنجليزية |
| منشور في: |
SAGE Publishing
2023-09-01
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| الوصول للمادة أونلاين: | https://doi.org/10.1177/00202940221145971 |
| _version_ | 1851941857119961088 |
|---|---|
| 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. |
| format | Article |
| id | doaj-art-09c7cbc7ff3f413dbd4cd50d93ca4864 |
| institution | Directory of Open Access Journals |
| issn | 0020-2940 |
| language | English |
| publishDate | 2023-09-01 |
| publisher | SAGE Publishing |
| record_format | Article |
| 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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