宇航学报

宇航学报 ›› 2022, Vol. 43 ›› Issue (4): 445-453.doi: 10.3873/j.issn.1000-1328.2022.04.006

• 制导、导航、控制与电子 • 上一篇    下一篇

一种低轨卫星高灵敏度辅助定位服务系统

王康，梁晟溟，董启甲，范广腾   

  1. 1. 航天恒星科技有限公司，北京 100095；2. 天津航天中为数据系统科技有限公司，天津 300301；3. 军事科学院国防科技创新研究院，北京 100071
  • 收稿日期:2021-05-13 修回日期:2021-08-13 出版日期:2022-04-15 发布日期:2022-04-15
  • 基金资助:
    国家自然科学基金(41974041)；国家自然科学基金青年基金(41801291，61806018)

A High Sensitivity Auxiliary Positioning Service System Using LEO Satellites

WANG Kang, LIANG Sheng ming, DONG Qi jia, FAN Guang teng   

  1. 1. Space Star Technology Co., Ltd, Beijing 100095, China;2. Tianjin Zhongwei Aerospace Data System Technology Co., Ltd, Tianjin 300301, China;3.National Innovation Institute of Defense Technology, Academy of Military Sciences, Beijing 100071, China
  • Received:2021-05-13 Revised:2021-08-13 Online:2022-04-15 Published:2022-04-15

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摘要： 本文针对全球导航卫星系统(GNSS)接收机低信噪比环境下的快速定位需求，在充分分析扩频信号相干积分关键影响要素的基础上，设计了一种低轨卫星高灵敏度辅助定位服务系统。针对空间段信号发射机低相噪信号生成技术所需的参考源、时钟树给出了详细设计及指标分析，通过发射信号误差向量幅度EVM对比测试，所设计的发射信号(EVM)指标可控制在优于1.19%。针对系统服务能力进行了星地一体化性能测试，实验结果表明，该系统可有效实现终端在灵敏度提升12 dB前提下有效定位且辅助定位时间优于3.5分钟。

关键词: 低轨卫星, 低相噪信号生成, 灵敏度, 辅助定位, 全球导航卫星系统

Abstract: Based on the analysis of the key factors affecting the coherent integration of spread spectrum signals, a novel high sensitivity auxiliary positioning service system for LEO satellite is proposed to address the fast positioning requirement of global navigation satellite system (GNSS) receivers under low signal to noise ratio environment. Detailed design and index analysis are given according to the reference source and clock tree for low phase noise signal generation technology in space segment signal transmitter. Error vector magnitude (EVM) comparison tests of the transmitted signal show that the EVM index can be controlled to be better than 1.19%. Furthermore, the satellite ground integration performance test is carried out in allusion to the system service capability, which shows the system can effectively realize the terminal positioning with the sensitivity increased by 12 dB, and the auxiliary positioning time is less than 3.5 minutes.

Key words: LEO satellite, Low phase noise signal generation, Sensitivity, Auxiliary positioning, Global navigation satellite system

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