一种低轨卫星载波相位差分定位方法

By selecting common-view satellites and establishing an EKF model for carrier phase differential positioning, the positioning error problem caused by the lack of orbital information of low-Earth orbit satellite signals was solved, thus improving the positioning accuracy of low-Earth orbit satellite navigation.

CN117949989BActive Publication Date: 2026-07-17BEIJING AUTOMATION CONTROL EQUIP INST

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
BEIJING AUTOMATION CONTROL EQUIP INST
Filing Date
2023-12-27
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Low-Earth orbit satellite signals do not contain or cannot extract orbital information of the radiation source, resulting in inconsistencies in the spatiotemporal reference in the positioning system. Existing technologies cannot effectively eliminate positioning errors caused by reference bias, leading to insufficient positioning accuracy.

Method used

By acquiring observation data from the base station and rover, common-view satellites are screened, a reference satellite is selected, an extended Kalman filter (EKF) model is established, and carrier phase differential positioning is performed to reduce the common error between the base station and the rover.

Benefits of technology

It improves the accuracy of low-orbit satellite navigation and positioning, reduces the positioning error between the base station and the rover, and achieves higher positioning accuracy.

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Abstract

本发明提供了一种低轨卫星载波相位差分定位方法,该低轨卫星载波相位差分定位方法包括:分别获取基准站接收机的观测量数据和流动站接收机的观测量数据,观测量数据包括载波相位观测量;获取基准站非差可用星列表和流动站非差可用星列表,从基准站非差可用星列表和流动站非差可用星列表中筛选共视星,并根据共视星的载波相位观测量筛选载波相位观测量单差可用星;从载波相位观测量单差可用星列表中选择基准星;根据载波相位观测量单差可用星和基准星进行EKF滤波,获取流动站的定位,完成低轨卫星载波相位差分定位。应用本发明的技术方案,能够解决现有技术中低轨卫星导航定位精度不足的技术问题。
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