Data-Driven Health Assessment in a Flight Control System under Uncertain Conditions
PHM technology plays an increasingly significant role in modern aviation condition-based maintenance. As an important part of prognostics and health management (PHM), a health assessment can effectively estimate the health status of a system and provide support for maintenance decision making. Howev...
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MDPI AG
2021
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oai:doaj.org-article:79a0d4d998a94782ac2cb472f2649eea2021-11-11T15:10:23ZData-Driven Health Assessment in a Flight Control System under Uncertain Conditions10.3390/app1121101072076-3417https://doaj.org/article/79a0d4d998a94782ac2cb472f2649eea2021-10-01T00:00:00Zhttps://www.mdpi.com/2076-3417/11/21/10107https://doaj.org/toc/2076-3417PHM technology plays an increasingly significant role in modern aviation condition-based maintenance. As an important part of prognostics and health management (PHM), a health assessment can effectively estimate the health status of a system and provide support for maintenance decision making. However, in actual conditions, various uncertain factors will amplify assessment errors and cause large fluctuations in assessment results. In this paper, uncertain factors are incorporated into flight control system health assessment modeling. First, four uncertain factors of health assessment characteristic parameters are quantified and described by the extended λ-PDF method to acquire their probability distribution function. Secondly, a Monte Carlo simulation (MCS) is used to simulate a flight control system health assessment process with uncertain factors. Thirdly, the probability distribution of the output health index is solved by the maximum entropy principle. Finally, the proposed model was verified with actual flight data. The comparison between assessment results with and without uncertain factors shows that a health assessment conducted under uncertain conditions can reduce the impact of the uncertainty of outliers on the assessment results and make the assessment results more stable; therefore, the false alarm rate can be reduced.Jie ChenYuyang ZhaoXiaofeng XueRunfeng ChenYingjian WuMDPI AGarticleaircraft systemcharacteristic parametersfuzzy comprehensive assessmentuncertainty qualificationλ-PDF probability densitymaximum entropyTechnologyTEngineering (General). Civil engineering (General)TA1-2040Biology (General)QH301-705.5PhysicsQC1-999ChemistryQD1-999ENApplied Sciences, Vol 11, Iss 10107, p 10107 (2021) |
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DOAJ |
language |
EN |
topic |
aircraft system characteristic parameters fuzzy comprehensive assessment uncertainty qualification λ-PDF probability density maximum entropy Technology T Engineering (General). Civil engineering (General) TA1-2040 Biology (General) QH301-705.5 Physics QC1-999 Chemistry QD1-999 |
spellingShingle |
aircraft system characteristic parameters fuzzy comprehensive assessment uncertainty qualification λ-PDF probability density maximum entropy Technology T Engineering (General). Civil engineering (General) TA1-2040 Biology (General) QH301-705.5 Physics QC1-999 Chemistry QD1-999 Jie Chen Yuyang Zhao Xiaofeng Xue Runfeng Chen Yingjian Wu Data-Driven Health Assessment in a Flight Control System under Uncertain Conditions |
description |
PHM technology plays an increasingly significant role in modern aviation condition-based maintenance. As an important part of prognostics and health management (PHM), a health assessment can effectively estimate the health status of a system and provide support for maintenance decision making. However, in actual conditions, various uncertain factors will amplify assessment errors and cause large fluctuations in assessment results. In this paper, uncertain factors are incorporated into flight control system health assessment modeling. First, four uncertain factors of health assessment characteristic parameters are quantified and described by the extended λ-PDF method to acquire their probability distribution function. Secondly, a Monte Carlo simulation (MCS) is used to simulate a flight control system health assessment process with uncertain factors. Thirdly, the probability distribution of the output health index is solved by the maximum entropy principle. Finally, the proposed model was verified with actual flight data. The comparison between assessment results with and without uncertain factors shows that a health assessment conducted under uncertain conditions can reduce the impact of the uncertainty of outliers on the assessment results and make the assessment results more stable; therefore, the false alarm rate can be reduced. |
format |
article |
author |
Jie Chen Yuyang Zhao Xiaofeng Xue Runfeng Chen Yingjian Wu |
author_facet |
Jie Chen Yuyang Zhao Xiaofeng Xue Runfeng Chen Yingjian Wu |
author_sort |
Jie Chen |
title |
Data-Driven Health Assessment in a Flight Control System under Uncertain Conditions |
title_short |
Data-Driven Health Assessment in a Flight Control System under Uncertain Conditions |
title_full |
Data-Driven Health Assessment in a Flight Control System under Uncertain Conditions |
title_fullStr |
Data-Driven Health Assessment in a Flight Control System under Uncertain Conditions |
title_full_unstemmed |
Data-Driven Health Assessment in a Flight Control System under Uncertain Conditions |
title_sort |
data-driven health assessment in a flight control system under uncertain conditions |
publisher |
MDPI AG |
publishDate |
2021 |
url |
https://doaj.org/article/79a0d4d998a94782ac2cb472f2649eea |
work_keys_str_mv |
AT jiechen datadrivenhealthassessmentinaflightcontrolsystemunderuncertainconditions AT yuyangzhao datadrivenhealthassessmentinaflightcontrolsystemunderuncertainconditions AT xiaofengxue datadrivenhealthassessmentinaflightcontrolsystemunderuncertainconditions AT runfengchen datadrivenhealthassessmentinaflightcontrolsystemunderuncertainconditions AT yingjianwu datadrivenhealthassessmentinaflightcontrolsystemunderuncertainconditions |
_version_ |
1718437151395282944 |