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"鹊桥"通导遥星座系统基于卫星时空信息的定位优化方法

李珍妮 陈立基 李茂登 陈旗鸣 何熊文 陈朝基 谢胜利

深空探测学报(中英文)2025,Vol.12Issue(4):377-390,14.
深空探测学报(中英文)2025,Vol.12Issue(4):377-390,14.DOI:10.3724/j.issn.2096-9287.2025.20250076

"鹊桥"通导遥星座系统基于卫星时空信息的定位优化方法

Positioning Optimization Method Based on Satellite Spatiotemporal Information for Queqiao Constellation System

李珍妮 1陈立基 1李茂登 2陈旗鸣 1何熊文 3陈朝基 3谢胜利1

作者信息

  • 1. 广东工业大学 自动化学院,广州 510006
  • 2. 深空探测实验室,北京 100195
  • 3. 北京空间飞行器总体设计部,北京 100094
  • 折叠

摘要

Abstract

Due to the fact that the number of visible satellites is limited,the finiteness of observation information and the ill-condition of the observation equation seriously constrain the positioning accuracy of the Least Squares(LS)method.To ad-dress this,a spatiotemporal information-enhanced LS positioning optimization method for future Queqiao communication-navigation-remote sensing constellation was proposed,aiming to improve the robustness of LS-based solutions.First,an auxil-iary equation incorporating multi-epoch pseudorange observations was constructed,coupled with a dynamic weighting strategy based on a constant-velocity motion model,to effectively utilize historical data and mitigate information deficiency in dynamic scenarios.Second,multi-epoch inter-satellite distance measurements are introduced to form geometric constraints that to sup-press ill-conditioning in the observation model.Finally,a Forward-Backward Smoother(FBS)algorithm was applied to further refine positioning results and enhance solution stability.Simulation experiments based on platform-generated orbital data of the Queqiao constellation demonstrate that,under a 10 m orbital error and with a historical epoch length of 19,the proposed method—fusing multi-epoch pseudorange and inter-satellite distance data with FBS smoothing—achieved a positioning accuracy of 7.03±2.50 m.Compared to the conventional LS method without any auxiliary information or smoothing,the positioning mean error was reduced by 88.26%and the standard deviation by 96.14%,providing solid technical support for high-precision posi-tioning and navigation services required for Chinese astronauts'lunar surface operations.

关键词

月轨卫星定位/最小二乘法/多历元观测数据融合/星间间距约束/双向滤波算法

Key words

lunar orbit satellite positioning/least squares method/multi-epoch observation data fusion/inter-satellite dis-tance constraint/Forward-Backward Smoother(FBS)algorithm

分类

天文与地球科学

引用本文复制引用

李珍妮,陈立基,李茂登,陈旗鸣,何熊文,陈朝基,谢胜利.."鹊桥"通导遥星座系统基于卫星时空信息的定位优化方法[J].深空探测学报(中英文),2025,12(4):377-390,14.

基金项目

民用航天技术预先研究项目(D040102) (D040102)

深空探测学报(中英文)

OA北大核心

2096-9287

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