A High-Precision Joint Smoothing Method for Interspacecraft Radio Frequency Doppler and Distance Measurements Using P-Spline Approximation

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2024-09-11 DOI:10.1109/TAES.2024.3458952
Jieyi Sun;Yongqing Wang;Yuyao Shen
{"title":"A High-Precision Joint Smoothing Method for Interspacecraft Radio Frequency Doppler and Distance Measurements Using P-Spline Approximation","authors":"Jieyi Sun;Yongqing Wang;Yuyao Shen","doi":"10.1109/TAES.2024.3458952","DOIUrl":null,"url":null,"abstract":"High-precision interspacecraft distance measurements obtained from radio frequency (RF) signals are essential for navigation processing methods (e.g., least squares and Kalman filter) in spacecraft formation and relative navigation applications. The joint smoothing of different measurements is an effective method for improving the precision of distance measurements. However, conventional methods (e.g., the Hatch filter) are primarily designed for Global Navigation Satellite System measurements obtained from terrestrial users. The smoothing models adopted in conventional methods exhibit poor dynamic adaptability, which hinders their ability to provide satisfactory precision. Therefore, this study proposes a joint smoothing method that applies a P-spline approximation to interspacecraft RF Doppler and distance measurements. To construct the smoothing model, the P-spline function was used because of its strong dynamic adaptability, favorable continuity, differentiability, and digital filter implementation structure. In addition, the formula for the differential property of the P-spline function was analyzed and proved. On this basis, Doppler measurements were incorporated into the smoothing model as a derivative of distance measurements, thereby increasing the precision of the distance measurements. Subsequently, the smoothing model was discretized. The core of the proposed method is the design of a P-spline smoother, which consisted of direct and indirect P-spline filters. To increase the antinoise performance, a 2-norm minimization criterion was introduced into the design of the direct P-spline filter. Furthermore, convolutional property was exploited to design the indirect P-spline filter. The simulation results indicated that the precision of the proposed P-spline smoother was superior to that of conventional methods.","PeriodicalId":13157,"journal":{"name":"IEEE Transactions on Aerospace and Electronic Systems","volume":"61 2","pages":"5315-5324"},"PeriodicalIF":5.7000,"publicationDate":"2024-09-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Transactions on Aerospace and Electronic Systems","FirstCategoryId":"94","ListUrlMain":"https://ieeexplore.ieee.org/document/10678846/","RegionNum":2,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

Abstract

High-precision interspacecraft distance measurements obtained from radio frequency (RF) signals are essential for navigation processing methods (e.g., least squares and Kalman filter) in spacecraft formation and relative navigation applications. The joint smoothing of different measurements is an effective method for improving the precision of distance measurements. However, conventional methods (e.g., the Hatch filter) are primarily designed for Global Navigation Satellite System measurements obtained from terrestrial users. The smoothing models adopted in conventional methods exhibit poor dynamic adaptability, which hinders their ability to provide satisfactory precision. Therefore, this study proposes a joint smoothing method that applies a P-spline approximation to interspacecraft RF Doppler and distance measurements. To construct the smoothing model, the P-spline function was used because of its strong dynamic adaptability, favorable continuity, differentiability, and digital filter implementation structure. In addition, the formula for the differential property of the P-spline function was analyzed and proved. On this basis, Doppler measurements were incorporated into the smoothing model as a derivative of distance measurements, thereby increasing the precision of the distance measurements. Subsequently, the smoothing model was discretized. The core of the proposed method is the design of a P-spline smoother, which consisted of direct and indirect P-spline filters. To increase the antinoise performance, a 2-norm minimization criterion was introduced into the design of the direct P-spline filter. Furthermore, convolutional property was exploited to design the indirect P-spline filter. The simulation results indicated that the precision of the proposed P-spline smoother was superior to that of conventional methods.
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
使用 P-样条逼近法的航天器间射频多普勒和距离测量高精度联合平滑法
在航天器编队和相关导航应用中,从射频信号中获得的高精度航天器间距离测量对于导航处理方法(如最小二乘法和卡尔曼滤波)至关重要。不同测量值的联合平滑是提高距离测量精度的有效方法。然而,传统方法(例如Hatch滤波器)主要是为从地面用户获得的全球导航卫星系统测量而设计的。传统方法采用的平滑模型动态适应性差,影响了其提供满意精度的能力。因此,本研究提出了一种联合平滑方法,该方法将p样条近似应用于航天器间射频多普勒和距离测量。由于p样条函数具有较强的动态适应性、良好的连续性、可微性和数字滤波器的实现结构,因此采用p样条函数构建平滑模型。此外,分析并证明了p样条函数的微分性质公式。在此基础上,将多普勒测量作为距离测量的导数纳入平滑模型,从而提高了距离测量的精度。随后,对平滑模型进行离散化处理。该方法的核心是p样条平滑器的设计,该光滑器由直接p样条滤波器和间接p样条滤波器组成。为了提高直接p样条滤波器的抗噪性能,在设计中引入了2范数最小化准则。此外,利用卷积特性设计了间接p样条滤波器。仿真结果表明,所提出的p样条光滑方法的精度优于传统的光滑方法。
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 去求助
来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
期刊最新文献
Safety-Critical Time-Synchronized Control for On-Orbit Approach to Rotating Targets Improved learning observer-based robust formation tracking control of helicopters under fixed and switching topologies A Probabilistic Ontology-Based Model for Multiple Aerial Target Threat Assessments in Short-Range Air Defense A Radio Frequency Interference Detection and Analytical Geolocation Method Demonstrated from LEO with an End-To-End Simulator and CYGNSS Raw Data Interrupted Sampling Repeater Jamming Suppression Based on Inter-pulse Frequency Coding LFM Signal and Mismatch Filter
×
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:604180095
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