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Intelligent Force-Measurement System Use in Shock Tunnel
The inertial vibration of the force measurement system (FMS) has a large influence on the force measuring result of aircraft, especially on some tests carried out in high-enthalpy impulse facilities, such as in a shock tunnel. When force tests are conducted in a shock tunnel, the low-frequency vibra...
Autores principales: | , |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
MDPI
2020
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7662283/ https://www.ncbi.nlm.nih.gov/pubmed/33142976 http://dx.doi.org/10.3390/s20216179 |
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author | Wang, Yunpeng Jiang, Zonglin |
author_facet | Wang, Yunpeng Jiang, Zonglin |
author_sort | Wang, Yunpeng |
collection | PubMed |
description | The inertial vibration of the force measurement system (FMS) has a large influence on the force measuring result of aircraft, especially on some tests carried out in high-enthalpy impulse facilities, such as in a shock tunnel. When force tests are conducted in a shock tunnel, the low-frequency vibrations of the FMS and its motion cannot be addressed through digital filtering because of the inertial forces, which are caused by the impact flow during the starting process of the shock tunnel. Therefore, this paper focuses on the dynamic characteristics of the performance of the FMS. A new method—i.e., deep-learning-based single-vector dynamic self-calibration (DL-based SV-DSC) of an impulse FMS, is proposed to increase the accuracy of aerodynamic force measurements in a shock tunnel. A deep-learning technique is used to train the dynamic model of the FMS in this study. Convolutional neural networks with a simple structure are applied to describe the dynamic modeling so that the low-frequency vibration signals are eliminated from the test results of the shock tunnel. By validation of the force test results measured in a shock tunnel, the current trained model can realize intelligent processing of the balance signals of the FMS. Based on this new method of dynamic calibration, the reliability and accuracy of force data processing are well verified. |
format | Online Article Text |
id | pubmed-7662283 |
institution | National Center for Biotechnology Information |
language | English |
publishDate | 2020 |
publisher | MDPI |
record_format | MEDLINE/PubMed |
spelling | pubmed-76622832020-11-14 Intelligent Force-Measurement System Use in Shock Tunnel Wang, Yunpeng Jiang, Zonglin Sensors (Basel) Article The inertial vibration of the force measurement system (FMS) has a large influence on the force measuring result of aircraft, especially on some tests carried out in high-enthalpy impulse facilities, such as in a shock tunnel. When force tests are conducted in a shock tunnel, the low-frequency vibrations of the FMS and its motion cannot be addressed through digital filtering because of the inertial forces, which are caused by the impact flow during the starting process of the shock tunnel. Therefore, this paper focuses on the dynamic characteristics of the performance of the FMS. A new method—i.e., deep-learning-based single-vector dynamic self-calibration (DL-based SV-DSC) of an impulse FMS, is proposed to increase the accuracy of aerodynamic force measurements in a shock tunnel. A deep-learning technique is used to train the dynamic model of the FMS in this study. Convolutional neural networks with a simple structure are applied to describe the dynamic modeling so that the low-frequency vibration signals are eliminated from the test results of the shock tunnel. By validation of the force test results measured in a shock tunnel, the current trained model can realize intelligent processing of the balance signals of the FMS. Based on this new method of dynamic calibration, the reliability and accuracy of force data processing are well verified. MDPI 2020-10-30 /pmc/articles/PMC7662283/ /pubmed/33142976 http://dx.doi.org/10.3390/s20216179 Text en © 2020 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 (http://creativecommons.org/licenses/by/4.0/). |
spellingShingle | Article Wang, Yunpeng Jiang, Zonglin Intelligent Force-Measurement System Use in Shock Tunnel |
title | Intelligent Force-Measurement System Use in Shock Tunnel |
title_full | Intelligent Force-Measurement System Use in Shock Tunnel |
title_fullStr | Intelligent Force-Measurement System Use in Shock Tunnel |
title_full_unstemmed | Intelligent Force-Measurement System Use in Shock Tunnel |
title_short | Intelligent Force-Measurement System Use in Shock Tunnel |
title_sort | intelligent force-measurement system use in shock tunnel |
topic | Article |
url | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7662283/ https://www.ncbi.nlm.nih.gov/pubmed/33142976 http://dx.doi.org/10.3390/s20216179 |
work_keys_str_mv | AT wangyunpeng intelligentforcemeasurementsystemuseinshocktunnel AT jiangzonglin intelligentforcemeasurementsystemuseinshocktunnel |