基于多普勒定位的低地轨道星座 GDOP 下限快速聚类卫星选择

IF 7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2024-08-26 DOI:10.1109/TAES.2024.3443021
Danyao Wang;Honglei Qin;Yu Zhang;Yibing Yang;Hongli Lv
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引用次数: 0

摘要

随着近地轨道(LEO)星座的快速发展,它们已成为传统全球卫星导航系统(GNSS)的有效补充,以满足定位需求。然而,由于可用卫星数量多,接收机硬件有限,无法充分利用所有可见卫星的信息,因此需要快速选择几何上优越的低轨道卫星组合进行定位。另一方面,由于低轨道卫星的非导航设计,通常采用基于多普勒测量的多历次定位,作为评估卫星组合的重要参数的几何精度稀释系数(GDOP)无法直接应用于传统GNSS常用的卫星选择方法。本文建立了低轨道卫星的多普勒- gdop (DGDOP)模型,并在此基础上提出了多普勒定位的快速聚类卫星选择方法。利用真实星链信号进行实验,结果表明,采用本文提出的FCSDp方法选择卫星组合进行定位,与传统方法相比,定位误差稳定降低45%以上,验证了该方法的有效性。采用本文提出的卫星选择方法进行低轨道卫星定位,可以保证较好的定位精度,同时满足较低的计算复杂度。
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Fast Clustering Satellite Selection Based on Doppler Positioning GDOP Lower Bound for LEO Constellation
With the rapid development of low Earth orbit (LEO) constellations, they have become an effective complement to the traditional global navigation satellite system (GNSS) in meeting positioning needs. However, the large number of available satellites and hardware limitations of the receivers make it impossible to fully apply the information from all visible satellites, hence it is necessary to quickly select a geometrically superior combination of LEO satellites for positioning. On the other hand, since the LEO satellites generally adopt multiple epochs positioning based on Doppler measurements due to their nonnavigation design, the geometric dilution of precision (GDOP), which is an important parameter for evaluating satellite combinations, and the common satellite selection methods in traditional GNSS cannot be applied directly. In this article, a Doppler-GDOP (DGDOP) model is developed for the LEO satellites, and a fast clustering satellite selection method for Doppler positioning (FCSDp) is proposed based on it. Experiments are performed using real Starlink signals, and the results show that using the FCSDp method proposed in this article to select satellite combinations for positioning could stably reduce the positioning error by more than 45% compared to the traditional method, which verifies the effectiveness of the method. Using the satellite selection method proposed in this article for LEO satellite positioning could ensure good positioning accuracy while satisfying low computational complexity.
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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.
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