滤波法与样条逼近法在飞行数据平滑中的比较

Q3 Earth and Planetary Sciences Aerospace Systems Pub Date : 2023-02-26 DOI:10.1007/s42401-023-00201-0
O. N. Korsun, Sekou Goro, M. H. Om
{"title":"滤波法与样条逼近法在飞行数据平滑中的比较","authors":"O. N. Korsun,&nbsp;Sekou Goro,&nbsp;M. H. Om","doi":"10.1007/s42401-023-00201-0","DOIUrl":null,"url":null,"abstract":"<div><p>Onboard measurement system, the function of which is to collect, record and process measurement information, performs these tasks by obtaining information from the sensors. However, the sensors are noisy, so it is necessary to combine multiple pieces of information to give a good accuracy to the signals provided by the onboard measurement system. The extended Kalman filter, which is one of the most widely used data fusion methods, is also one of the derivatives of the standard Kalman filter used for non-linear problems. On the other hand, the spline approximation, especially the cubic and Hermitian splines provide a very good and smooth estimate. It is known that the implementation of spline method is simpler than Kalman filtering. This paper describes an empirical comparative analysis of the extended Kalman filter and spline method. The impressive result is that a simple spline approximation in many cases performs better than a sophisticated Kalman filter.</p></div>","PeriodicalId":36309,"journal":{"name":"Aerospace Systems","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"2023-02-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"A comparison between filtering approach and spline approximation method in smoothing flight data\",\"authors\":\"O. N. Korsun,&nbsp;Sekou Goro,&nbsp;M. H. Om\",\"doi\":\"10.1007/s42401-023-00201-0\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>Onboard measurement system, the function of which is to collect, record and process measurement information, performs these tasks by obtaining information from the sensors. However, the sensors are noisy, so it is necessary to combine multiple pieces of information to give a good accuracy to the signals provided by the onboard measurement system. The extended Kalman filter, which is one of the most widely used data fusion methods, is also one of the derivatives of the standard Kalman filter used for non-linear problems. On the other hand, the spline approximation, especially the cubic and Hermitian splines provide a very good and smooth estimate. It is known that the implementation of spline method is simpler than Kalman filtering. This paper describes an empirical comparative analysis of the extended Kalman filter and spline method. The impressive result is that a simple spline approximation in many cases performs better than a sophisticated Kalman filter.</p></div>\",\"PeriodicalId\":36309,\"journal\":{\"name\":\"Aerospace Systems\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2023-02-26\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Aerospace Systems\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://link.springer.com/article/10.1007/s42401-023-00201-0\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q3\",\"JCRName\":\"Earth and Planetary Sciences\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Systems","FirstCategoryId":"1085","ListUrlMain":"https://link.springer.com/article/10.1007/s42401-023-00201-0","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"Earth and Planetary Sciences","Score":null,"Total":0}
引用次数: 1

摘要

车载测量系统的功能是收集、记录和处理测量信息,通过从传感器获取信息来执行这些任务。然而,传感器有噪声,因此有必要将多条信息组合起来,以使车载测量系统提供的信号具有良好的准确性。扩展卡尔曼滤波器是应用最广泛的数据融合方法之一,也是用于非线性问题的标准卡尔曼滤波器的导数之一。另一方面,样条逼近,特别是三次样条和埃尔米特样条提供了非常好的平滑估计。众所周知,样条方法的实现比卡尔曼滤波更简单。本文介绍了扩展卡尔曼滤波器和样条法的经验比较分析。令人印象深刻的结果是,在许多情况下,简单的样条近似比复杂的卡尔曼滤波器表现得更好。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
A comparison between filtering approach and spline approximation method in smoothing flight data

Onboard measurement system, the function of which is to collect, record and process measurement information, performs these tasks by obtaining information from the sensors. However, the sensors are noisy, so it is necessary to combine multiple pieces of information to give a good accuracy to the signals provided by the onboard measurement system. The extended Kalman filter, which is one of the most widely used data fusion methods, is also one of the derivatives of the standard Kalman filter used for non-linear problems. On the other hand, the spline approximation, especially the cubic and Hermitian splines provide a very good and smooth estimate. It is known that the implementation of spline method is simpler than Kalman filtering. This paper describes an empirical comparative analysis of the extended Kalman filter and spline method. The impressive result is that a simple spline approximation in many cases performs better than a sophisticated Kalman filter.

求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
Aerospace Systems
Aerospace Systems Social Sciences-Social Sciences (miscellaneous)
CiteScore
1.80
自引率
0.00%
发文量
53
期刊介绍: Aerospace Systems provides an international, peer-reviewed forum which focuses on system-level research and development regarding aeronautics and astronautics. The journal emphasizes the unique role and increasing importance of informatics on aerospace. It fills a gap in current publishing coverage from outer space vehicles to atmospheric vehicles by highlighting interdisciplinary science, technology and engineering. Potential topics include, but are not limited to: Trans-space vehicle systems design and integration Air vehicle systems Space vehicle systems Near-space vehicle systems Aerospace robotics and unmanned system Communication, navigation and surveillance Aerodynamics and aircraft design Dynamics and control Aerospace propulsion Avionics system Opto-electronic system Air traffic management Earth observation Deep space exploration Bionic micro-aircraft/spacecraft Intelligent sensing and Information fusion
期刊最新文献
Trajectory prediction for fighter aircraft ground collision avoidance based on the model predictive control technique Initial gap modeling for wing assembly analysis A survey on synthetic jets as active flow control Deconvolution of mode composition beamforming for rotating source localization Computational study on effect of free-stream turbulence on bio-inspired corrugated airfoil at different sections at low Reynolds number
×
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
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 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 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1