LSTM based prediction algorithm and abnormal change detection for temperature in aerospace gyroscope shell
Purpose Abnormal changes in temperature directly affect the stability and reliability of a gyroscope. Predicting the temperature and detecting the abnormal change is great value for timely understanding of the working state of the gyroscope. Considering that the actual collected gyroscope shell temp...
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Veröffentlicht in: | International journal of intelligent computing and cybernetics 2019-05, Vol.12 (2), p.274-291 |
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creator | Shi, Haoqiang Hu, Shaolin Zhang, Jiaxu |
description | Purpose
Abnormal changes in temperature directly affect the stability and reliability of a gyroscope. Predicting the temperature and detecting the abnormal change is great value for timely understanding of the working state of the gyroscope. Considering that the actual collected gyroscope shell temperature data have strong non-linearity and are accompanied by random noise pollution, the prediction accuracy and convergence speed of the traditional method need to be improved. The purpose of this paper is to use a predictive model with strong nonlinear mapping ability to predict the temperature of the gyroscope to improve the prediction accuracy and detect the abnormal change.
Design/methodology/approach
In this paper, an double hidden layer long-short term memory (LSTM) is presented to predict temperature data for the gyroscope (including single point and period prediction), and the evaluation index of the prediction effect is also proposed, and the prediction effects of shell temperature data are compared by BP network, support vector machine (SVM) and LSTM network. Using the estimated value detects the abnormal change of the gyroscope.
Findings
By combined simulation calculation with the gyroscope measured data, the effect of different network hyperparameters on shell temperature prediction of the gyroscope is analyzed, and the LSTM network can be used to predict the temperature (time series data). By comparing the performance indicators of different prediction methods, the accuracy of the shell temperature estimation by LSTM is better, which can meet the requirements of abnormal change detection. Quick and accurate diagnosis of different types of gyroscope faults (steps and drifts) can be achieved by setting reasonable data window lengths and thresholds.
Practical implications
The LSTM model is a deep neural network model with multiple non-linear mapping levels, and can abstract the input signal layer by layer and extract features to discover deeper underlying laws. The improved method has been used to solve the problem of strong non-linearity and random noise pollution in time series, and the estimated value can detect the abnormal change of the gyroscope.
Originality/value
In this paper, based on the LSTM network, an double hidden layer LSTM is presented to predict temperature data for the gyroscope (including single point and period prediction), and validate the effectiveness and feasibility of the algorithm by using shell temperature measurement data. |
doi_str_mv | 10.1108/IJICC-11-2018-0152 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2224998676</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2224998676</sourcerecordid><originalsourceid>FETCH-LOGICAL-c317t-b6a50e0b3b3a5ab48b6182d238afb20a49efc9097d5e037e47502f4213537cea3</originalsourceid><addsrcrecordid>eNptkTtPwzAUhS0EEqXwB5gsMQf8iGNnRBWPoiIGisRm2c5NmyqJg50O_HtcgpCQmO4Zzncf5yJ0Sck1pUTdLJ-Wi0VGacYIVRmhgh2hGZWiyLgs1fGvVu-n6CzGHSGFEorP0G71un7G1kSo8BCgatzY-B6bduNDM247bPoKG9v70JkWu63pN4ArGGHy1T7gEboBghn3AXCTUAg-DsYB3nwm5fwAOG6hbc_RSW3aCBc_dY7e7u_Wi8ds9fKwXNyuMsepHDNbGEGAWG65EcbmyhZUsYpxZWrLiMlLqF1JSlkJIFxCLgVhdc4oF1w6MHyOrqa-Q_Afe4ij3vl96NNIzRjLy1IVskguNrlcWjIGqPUQms6ET02JPmSqvzNNUh8y1YdME0QnCLp0cVv9z_z5A_8CIaJ56Q</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2224998676</pqid></control><display><type>article</type><title>LSTM based prediction algorithm and abnormal change detection for temperature in aerospace gyroscope shell</title><source>Emerald Journals</source><source>Standard: Emerald eJournal Premier Collection</source><creator>Shi, Haoqiang ; Hu, Shaolin ; Zhang, Jiaxu</creator><creatorcontrib>Shi, Haoqiang ; Hu, Shaolin ; Zhang, Jiaxu</creatorcontrib><description>Purpose
Abnormal changes in temperature directly affect the stability and reliability of a gyroscope. Predicting the temperature and detecting the abnormal change is great value for timely understanding of the working state of the gyroscope. Considering that the actual collected gyroscope shell temperature data have strong non-linearity and are accompanied by random noise pollution, the prediction accuracy and convergence speed of the traditional method need to be improved. The purpose of this paper is to use a predictive model with strong nonlinear mapping ability to predict the temperature of the gyroscope to improve the prediction accuracy and detect the abnormal change.
Design/methodology/approach
In this paper, an double hidden layer long-short term memory (LSTM) is presented to predict temperature data for the gyroscope (including single point and period prediction), and the evaluation index of the prediction effect is also proposed, and the prediction effects of shell temperature data are compared by BP network, support vector machine (SVM) and LSTM network. Using the estimated value detects the abnormal change of the gyroscope.
Findings
By combined simulation calculation with the gyroscope measured data, the effect of different network hyperparameters on shell temperature prediction of the gyroscope is analyzed, and the LSTM network can be used to predict the temperature (time series data). By comparing the performance indicators of different prediction methods, the accuracy of the shell temperature estimation by LSTM is better, which can meet the requirements of abnormal change detection. Quick and accurate diagnosis of different types of gyroscope faults (steps and drifts) can be achieved by setting reasonable data window lengths and thresholds.
Practical implications
The LSTM model is a deep neural network model with multiple non-linear mapping levels, and can abstract the input signal layer by layer and extract features to discover deeper underlying laws. The improved method has been used to solve the problem of strong non-linearity and random noise pollution in time series, and the estimated value can detect the abnormal change of the gyroscope.
Originality/value
In this paper, based on the LSTM network, an double hidden layer LSTM is presented to predict temperature data for the gyroscope (including single point and period prediction), and validate the effectiveness and feasibility of the algorithm by using shell temperature measurement data. The prediction effects of shell temperature data are compared by BP network, SVM and LSTM network. The LSTM network has the best prediction effect, and is used to predict the temperature of the gyroscope to improve the prediction accuracy and detect the abnormal change.</description><identifier>ISSN: 1756-378X</identifier><identifier>EISSN: 1756-3798</identifier><identifier>DOI: 10.1108/IJICC-11-2018-0152</identifier><language>eng</language><publisher>Bingley: Emerald Publishing Limited</publisher><subject>Accuracy ; Algorithms ; Artificial neural networks ; Business metrics ; Change detection ; Computer simulation ; Deep learning ; Fault detection ; Fault diagnosis ; Feature extraction ; Linearity ; Mapping ; Mathematical models ; Navigation systems ; Neural networks ; Noise pollution ; Noise prediction ; Nonlinearity ; Parameter identification ; Random noise ; Shell stability ; Support vector machines ; Temperature measurement ; Time series</subject><ispartof>International journal of intelligent computing and cybernetics, 2019-05, Vol.12 (2), p.274-291</ispartof><rights>Emerald Publishing Limited</rights><rights>Emerald Publishing Limited 2019</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c317t-b6a50e0b3b3a5ab48b6182d238afb20a49efc9097d5e037e47502f4213537cea3</citedby><cites>FETCH-LOGICAL-c317t-b6a50e0b3b3a5ab48b6182d238afb20a49efc9097d5e037e47502f4213537cea3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.emerald.com/insight/content/doi/10.1108/IJICC-11-2018-0152/full/html$$EHTML$$P50$$Gemerald$$H</linktohtml><link.rule.ids>314,776,780,961,11615,21675,27902,27903,52666,53221</link.rule.ids></links><search><creatorcontrib>Shi, Haoqiang</creatorcontrib><creatorcontrib>Hu, Shaolin</creatorcontrib><creatorcontrib>Zhang, Jiaxu</creatorcontrib><title>LSTM based prediction algorithm and abnormal change detection for temperature in aerospace gyroscope shell</title><title>International journal of intelligent computing and cybernetics</title><description>Purpose
Abnormal changes in temperature directly affect the stability and reliability of a gyroscope. Predicting the temperature and detecting the abnormal change is great value for timely understanding of the working state of the gyroscope. Considering that the actual collected gyroscope shell temperature data have strong non-linearity and are accompanied by random noise pollution, the prediction accuracy and convergence speed of the traditional method need to be improved. The purpose of this paper is to use a predictive model with strong nonlinear mapping ability to predict the temperature of the gyroscope to improve the prediction accuracy and detect the abnormal change.
Design/methodology/approach
In this paper, an double hidden layer long-short term memory (LSTM) is presented to predict temperature data for the gyroscope (including single point and period prediction), and the evaluation index of the prediction effect is also proposed, and the prediction effects of shell temperature data are compared by BP network, support vector machine (SVM) and LSTM network. Using the estimated value detects the abnormal change of the gyroscope.
Findings
By combined simulation calculation with the gyroscope measured data, the effect of different network hyperparameters on shell temperature prediction of the gyroscope is analyzed, and the LSTM network can be used to predict the temperature (time series data). By comparing the performance indicators of different prediction methods, the accuracy of the shell temperature estimation by LSTM is better, which can meet the requirements of abnormal change detection. Quick and accurate diagnosis of different types of gyroscope faults (steps and drifts) can be achieved by setting reasonable data window lengths and thresholds.
Practical implications
The LSTM model is a deep neural network model with multiple non-linear mapping levels, and can abstract the input signal layer by layer and extract features to discover deeper underlying laws. The improved method has been used to solve the problem of strong non-linearity and random noise pollution in time series, and the estimated value can detect the abnormal change of the gyroscope.
Originality/value
In this paper, based on the LSTM network, an double hidden layer LSTM is presented to predict temperature data for the gyroscope (including single point and period prediction), and validate the effectiveness and feasibility of the algorithm by using shell temperature measurement data. The prediction effects of shell temperature data are compared by BP network, SVM and LSTM network. The LSTM network has the best prediction effect, and is used to predict the temperature of the gyroscope to improve the prediction accuracy and detect the abnormal change.</description><subject>Accuracy</subject><subject>Algorithms</subject><subject>Artificial neural networks</subject><subject>Business metrics</subject><subject>Change detection</subject><subject>Computer simulation</subject><subject>Deep learning</subject><subject>Fault detection</subject><subject>Fault diagnosis</subject><subject>Feature extraction</subject><subject>Linearity</subject><subject>Mapping</subject><subject>Mathematical models</subject><subject>Navigation systems</subject><subject>Neural networks</subject><subject>Noise pollution</subject><subject>Noise prediction</subject><subject>Nonlinearity</subject><subject>Parameter identification</subject><subject>Random noise</subject><subject>Shell stability</subject><subject>Support vector machines</subject><subject>Temperature measurement</subject><subject>Time series</subject><issn>1756-378X</issn><issn>1756-3798</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><sourceid>BENPR</sourceid><recordid>eNptkTtPwzAUhS0EEqXwB5gsMQf8iGNnRBWPoiIGisRm2c5NmyqJg50O_HtcgpCQmO4Zzncf5yJ0Sck1pUTdLJ-Wi0VGacYIVRmhgh2hGZWiyLgs1fGvVu-n6CzGHSGFEorP0G71un7G1kSo8BCgatzY-B6bduNDM247bPoKG9v70JkWu63pN4ArGGHy1T7gEboBghn3AXCTUAg-DsYB3nwm5fwAOG6hbc_RSW3aCBc_dY7e7u_Wi8ds9fKwXNyuMsepHDNbGEGAWG65EcbmyhZUsYpxZWrLiMlLqF1JSlkJIFxCLgVhdc4oF1w6MHyOrqa-Q_Afe4ij3vl96NNIzRjLy1IVskguNrlcWjIGqPUQms6ET02JPmSqvzNNUh8y1YdME0QnCLp0cVv9z_z5A_8CIaJ56Q</recordid><startdate>20190515</startdate><enddate>20190515</enddate><creator>Shi, Haoqiang</creator><creator>Hu, Shaolin</creator><creator>Zhang, Jiaxu</creator><general>Emerald Publishing Limited</general><general>Emerald Group Publishing Limited</general><scope>AAYXX</scope><scope>CITATION</scope><scope>0U~</scope><scope>1-H</scope><scope>7SC</scope><scope>7WY</scope><scope>7WZ</scope><scope>7XB</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BEZIV</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>F~G</scope><scope>GNUQQ</scope><scope>HCIFZ</scope><scope>JQ2</scope><scope>K6~</scope><scope>K7-</scope><scope>L.-</scope><scope>L.0</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><scope>M0C</scope><scope>M0N</scope><scope>M2P</scope><scope>P5Z</scope><scope>P62</scope><scope>PQBIZ</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PYYUZ</scope><scope>Q9U</scope></search><sort><creationdate>20190515</creationdate><title>LSTM based prediction algorithm and abnormal change detection for temperature in aerospace gyroscope shell</title><author>Shi, Haoqiang ; Hu, Shaolin ; Zhang, Jiaxu</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c317t-b6a50e0b3b3a5ab48b6182d238afb20a49efc9097d5e037e47502f4213537cea3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Accuracy</topic><topic>Algorithms</topic><topic>Artificial neural networks</topic><topic>Business metrics</topic><topic>Change detection</topic><topic>Computer simulation</topic><topic>Deep learning</topic><topic>Fault detection</topic><topic>Fault diagnosis</topic><topic>Feature extraction</topic><topic>Linearity</topic><topic>Mapping</topic><topic>Mathematical models</topic><topic>Navigation systems</topic><topic>Neural networks</topic><topic>Noise pollution</topic><topic>Noise prediction</topic><topic>Nonlinearity</topic><topic>Parameter identification</topic><topic>Random noise</topic><topic>Shell stability</topic><topic>Support vector machines</topic><topic>Temperature measurement</topic><topic>Time series</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Shi, Haoqiang</creatorcontrib><creatorcontrib>Hu, Shaolin</creatorcontrib><creatorcontrib>Zhang, Jiaxu</creatorcontrib><collection>CrossRef</collection><collection>Global News & ABI/Inform Professional</collection><collection>Trade PRO</collection><collection>Computer and Information Systems Abstracts</collection><collection>ABI/INFORM Collection</collection><collection>ABI/INFORM Global (PDF only)</collection><collection>ProQuest Central (purchase pre-March 2016)</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central UK/Ireland</collection><collection>Advanced Technologies & Aerospace Collection</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Business Premium Collection</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>ABI/INFORM Global (Corporate)</collection><collection>ProQuest Central Student</collection><collection>SciTech Premium Collection</collection><collection>ProQuest Computer Science Collection</collection><collection>ProQuest Business Collection</collection><collection>Computer Science Database</collection><collection>ABI/INFORM Professional Advanced</collection><collection>ABI/INFORM Professional Standard</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><collection>ABI/INFORM Global</collection><collection>Computing Database</collection><collection>Science Database</collection><collection>Advanced Technologies & Aerospace Database</collection><collection>ProQuest Advanced Technologies & Aerospace Collection</collection><collection>ProQuest One Business</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ABI/INFORM Collection China</collection><collection>ProQuest Central Basic</collection><jtitle>International journal of intelligent computing and cybernetics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Shi, Haoqiang</au><au>Hu, Shaolin</au><au>Zhang, Jiaxu</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>LSTM based prediction algorithm and abnormal change detection for temperature in aerospace gyroscope shell</atitle><jtitle>International journal of intelligent computing and cybernetics</jtitle><date>2019-05-15</date><risdate>2019</risdate><volume>12</volume><issue>2</issue><spage>274</spage><epage>291</epage><pages>274-291</pages><issn>1756-378X</issn><eissn>1756-3798</eissn><abstract>Purpose
Abnormal changes in temperature directly affect the stability and reliability of a gyroscope. Predicting the temperature and detecting the abnormal change is great value for timely understanding of the working state of the gyroscope. Considering that the actual collected gyroscope shell temperature data have strong non-linearity and are accompanied by random noise pollution, the prediction accuracy and convergence speed of the traditional method need to be improved. The purpose of this paper is to use a predictive model with strong nonlinear mapping ability to predict the temperature of the gyroscope to improve the prediction accuracy and detect the abnormal change.
Design/methodology/approach
In this paper, an double hidden layer long-short term memory (LSTM) is presented to predict temperature data for the gyroscope (including single point and period prediction), and the evaluation index of the prediction effect is also proposed, and the prediction effects of shell temperature data are compared by BP network, support vector machine (SVM) and LSTM network. Using the estimated value detects the abnormal change of the gyroscope.
Findings
By combined simulation calculation with the gyroscope measured data, the effect of different network hyperparameters on shell temperature prediction of the gyroscope is analyzed, and the LSTM network can be used to predict the temperature (time series data). By comparing the performance indicators of different prediction methods, the accuracy of the shell temperature estimation by LSTM is better, which can meet the requirements of abnormal change detection. Quick and accurate diagnosis of different types of gyroscope faults (steps and drifts) can be achieved by setting reasonable data window lengths and thresholds.
Practical implications
The LSTM model is a deep neural network model with multiple non-linear mapping levels, and can abstract the input signal layer by layer and extract features to discover deeper underlying laws. The improved method has been used to solve the problem of strong non-linearity and random noise pollution in time series, and the estimated value can detect the abnormal change of the gyroscope.
Originality/value
In this paper, based on the LSTM network, an double hidden layer LSTM is presented to predict temperature data for the gyroscope (including single point and period prediction), and validate the effectiveness and feasibility of the algorithm by using shell temperature measurement data. The prediction effects of shell temperature data are compared by BP network, SVM and LSTM network. The LSTM network has the best prediction effect, and is used to predict the temperature of the gyroscope to improve the prediction accuracy and detect the abnormal change.</abstract><cop>Bingley</cop><pub>Emerald Publishing Limited</pub><doi>10.1108/IJICC-11-2018-0152</doi><tpages>18</tpages></addata></record> |
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subjects | Accuracy Algorithms Artificial neural networks Business metrics Change detection Computer simulation Deep learning Fault detection Fault diagnosis Feature extraction Linearity Mapping Mathematical models Navigation systems Neural networks Noise pollution Noise prediction Nonlinearity Parameter identification Random noise Shell stability Support vector machines Temperature measurement Time series |
title | LSTM based prediction algorithm and abnormal change detection for temperature in aerospace gyroscope shell |
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