深空探测学报（中英文）2025，Vol.12Issue(2)：144-152,9.DOI:10.15982/j.issn.2096-9287.2025.20250005
一种木星探测器天文测角/相对论组合导航方法
A Star Angle/StarNAV Integrated Navigation Method for Jupiter Exploration
桂明臻 1张展赫 1熊凯 2宁晓琳3
作者信息
- 1. 中南大学 自动化学院,长沙 410083||光电智能测控湖南省重点实验室,长沙 410083
- 2. 北京控制工程研究所,北京 100094
- 3. 北京航空航天大学 仪器科学与光电工程学院,北京 100191
- 折叠
摘要
Abstract
Due to Jupiter's long distance from us,the positional error of Jupiter can reach hundreds of kilometers,posing significant challenges to autonomous navigation for spacecraft.To address this issue,a star angle/StarNAV integrated navigation method was proposed.By analyzing the impact of ephemeris error of Jupiter on StarNAV,it was observed that velocity error of Jupiter had a greater influence on StarNAV,while positional error had a relatively smaller effect.Considering that Jupiter's positional error is relatively large while its velocity error was small,the integration of star angle navigation and StarNAV was applied to Jupiter exploration.In this method,Star Angle navigation provides the spacecraft's position relative to Jupiter,while StarNAV primarily supplies the velocity information of the spacecraft's relative to Jupiter.Simulation results demonstrate that the proposed integrated navigation method is nearly unaffected by Jupiter's ephemeris error and achieves significantly higher accuracy than Star Angle navigation or StarNAV alone,providing high-precision autonomous navigation information for Jupiter exploration.关键词
木星探测/自主导航/星历误差/组合导航Key words
Jupiter exploration/autonomous navigation/ephemeris error/integrated navigation分类
航空航天引用本文复制引用
桂明臻,张展赫,熊凯,宁晓琳..一种木星探测器天文测角/相对论组合导航方法[J].深空探测学报（中英文）,2025,12(2):144-152,9.
