A NEW METHOD IN CONCEPTUAL DESIGN OF THE SHM AIRFRAME USING ROUGH SETS

K. Kustroń
{"title":"A NEW METHOD IN CONCEPTUAL DESIGN OF THE SHM AIRFRAME USING ROUGH SETS","authors":"K. Kustroń","doi":"10.12783/shm2021/36354","DOIUrl":null,"url":null,"abstract":"A very promising solution in airframe design is a new trend in application based on intelligent online condition monitoring known as Structural Condition/Health Monitoring/Management System, which has evolved towards Integrated System Health Management to cover the whole System-of-Systems architecture. This paper focuses on how to reduce Big Data with reference to a comprehensive model for designing future airframe heath monitoring system, including the problem of assessing the diversity of various sensors used in the assessment of the technical condition/health of an airframe, which generates big data sets with different records of measurement data that must be reduced for effective using. The paper summarizes the research on the assessment of sensors in terms of their suitability and effectiveness in monitoring the airframe condition, including metal and composite, and refers to the complexity of the problem by integrating the technical condition/health of the engine unit and the airframe. Integration issue of the reliability serial connection of the airframe and engine for airworthiness assessment were mentioned. A new method based on the rough set paradigm, including hybrid variants, for the reduction of big data of health monitoring into their effective management were postulated and advantages were demonstrated. The proposed method in the form of listed issues is complementary to the currently used method and is aimed at supporting the design of the airframe at the preliminary assessment stage. That method is strongly recommended to increase security and reduce computational cost and operational cost including maintenance cost in aircraft life-cycle costs.","PeriodicalId":180083,"journal":{"name":"Proceedings of the 13th International Workshop on Structural Health Monitoring","volume":"29 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-03-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the 13th International Workshop on Structural Health Monitoring","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.12783/shm2021/36354","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

A very promising solution in airframe design is a new trend in application based on intelligent online condition monitoring known as Structural Condition/Health Monitoring/Management System, which has evolved towards Integrated System Health Management to cover the whole System-of-Systems architecture. This paper focuses on how to reduce Big Data with reference to a comprehensive model for designing future airframe heath monitoring system, including the problem of assessing the diversity of various sensors used in the assessment of the technical condition/health of an airframe, which generates big data sets with different records of measurement data that must be reduced for effective using. The paper summarizes the research on the assessment of sensors in terms of their suitability and effectiveness in monitoring the airframe condition, including metal and composite, and refers to the complexity of the problem by integrating the technical condition/health of the engine unit and the airframe. Integration issue of the reliability serial connection of the airframe and engine for airworthiness assessment were mentioned. A new method based on the rough set paradigm, including hybrid variants, for the reduction of big data of health monitoring into their effective management were postulated and advantages were demonstrated. The proposed method in the form of listed issues is complementary to the currently used method and is aimed at supporting the design of the airframe at the preliminary assessment stage. That method is strongly recommended to increase security and reduce computational cost and operational cost including maintenance cost in aircraft life-cycle costs.
基于粗糙集的SHM机身概念设计新方法
基于智能在线状态监测的结构状态/健康监测/管理系统是机身设计中一个非常有前途的解决方案,该系统已向集成系统健康管理发展,涵盖了整个系统的体系结构。本文的重点是如何减少大数据,参考一个综合模型来设计未来的机体健康监测系统,包括评估机体技术状态/健康评估中使用的各种传感器的多样性问题,这些传感器产生的大数据集具有不同的测量数据记录,必须进行减少才能有效使用。本文总结了金属和复合材料传感器在机体状态监测中的适用性和有效性评估研究,并将发动机和机体的技术状态/健康状况结合起来,指出了问题的复杂性。提出了适航评定中机体与发动机可靠性串行连接的集成问题。提出了一种基于包括混合变量在内的粗糙集范式的健康监测大数据化简有效管理的新方法,并证明了该方法的优越性。以列出问题的形式提出的方法是对目前使用的方法的补充,旨在支持初步评估阶段的机身设计。强烈建议使用这种方法来提高安全性,降低计算成本和运营成本,包括飞机生命周期成本中的维护成本。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信