Accuracy analysis of orbit determination for high Earth orbit gravitational wave detectors using multi-GNSS sidelobe signals

IF 3.4 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE Acta Astronautica Pub Date : 2025-01-23 DOI:10.1016/j.actaastro.2025.01.022
Lisheng Tong , Kai Shao , Defeng Gu , Chengjun Yang , Chunbo Wei , Zicong An , Zheyu Xu , Jubo Zhu , Jian Wang , Daoping Liu
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Abstract

It is critical to maintain high-precision orbit determination in high Earth orbit gravitational wave detectors. The TianQin space-borne gravitational wave detector, a typical high Earth orbit satellite constellation, utilises an equilateral triangular satellite formation design. This paper presents the first study of the orbit determination of TianQin by utilising global navigation satellite system (GNSS) sidelobe signals through simulation. The number of visible GNSS satellites, tracking performance, position dilution of precision (PDOP), single point positioning (SPP) accuracy, and precise orbit determination (POD) accuracy of the TianQin satellites are comprehensively analysed to provide a reference for subsequent scientific tasks. The conclusions are as follows: (1) Due to the high orbit of the TianQin satellites, the signal intensity is weak, resulting in reduced visibility, narrower elevation angles of the visible antenna, and more prominent geometric accuracy factors. Therefore, utilising multi-GNSS systems and side lobe signals for orbit determination is necessary. (2) The receiver’s signal reception threshold plays a crucial role. Higher receiver sensitivity enhances the positioning and orbit determination performances of the TianQin satellites. (3) With a signal reception threshold setting of -159 dBm, the SPP accuracy of the TianQin satellites using the four GNSS system configurations is 153.81 m. (4) With a signal reception threshold set to -159 dBm, the four GNSS systems can fulfil TianQin’s orbit determination accuracy requirements of 5 m for radial position and 2 mm/s for along-track velocity within a 7-day arc length. TianQin’s position accuracy is 12.27 m for the 3-dimensional (3D) direction and 4.02 m for the radial direction, and the velocity accuracy is 0.65 mm/s for the 3D direction and 0.15 mm/s for the along-track direction.
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基于多gnss旁瓣信号的高地球轨道引力波探测器定轨精度分析
在高地球轨道引力波探测器中,保持高精度定轨是至关重要的。天勤星载引力波探测器是一个典型的高地球轨道卫星星座,采用等边三角形卫星编队设计。本文首次通过仿真研究了利用全球导航卫星系统(GNSS)旁瓣信号确定天琴卫星轨道的方法。综合分析了天秦卫星的GNSS可见卫星数量、跟踪性能、位置精度稀释(PDOP)、单点定位(SPP)精度和精确定轨(POD)精度,为后续科学任务提供参考。研究结果表明:(1)由于天琴卫星的高轨道,信号强度较弱,导致能见度降低,可见天线仰角变窄,几何精度因素更加突出。因此,利用多gnss系统和旁瓣信号进行定轨是必要的。(2)接收机的信号接收阈值起着至关重要的作用。接收机灵敏度的提高提高了天琴卫星的定位定轨性能。(3)当信号接收阈值设置为-159 dBm时,4种GNSS系统配置的天琴卫星SPP精度为153.81 m。(4)当信号接收阈值设置为-159 dBm时,4种GNSS系统可以满足天琴卫星在7天弧长内径向位置5 m、沿轨速度2 mm/s的定轨精度要求。天琴的定位精度在三维方向为12.27 m,径向为4.02 m,速度精度在三维方向为0.65 mm/s,沿轨道方向为0.15 mm/s。
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来源期刊
Acta Astronautica
Acta Astronautica 工程技术-工程:宇航
CiteScore
7.20
自引率
22.90%
发文量
599
审稿时长
53 days
期刊介绍: Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to: The peaceful scientific exploration of space, Its exploitation for human welfare and progress, Conception, design, development and operation of space-borne and Earth-based systems, In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.
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