Precision analysis of autonomous orbit determination using star sensor for Beidou MEO satellite

被引：8

作者：

Shang, Lin ^{[1
]}

Chang, Jiachao ^{[1
,2
,3
]}

Zhang, Jun ^{[1
]}

Li, Guotong ^{[1
,4
]}

机构：

[1] Shanghai Engn Ctr Microsatellites, Room 4502,99,Haike Rd, Shanghai, Peoples R China

[2] Chinese Acad Sci, Shanghai Inst Microsyst & Informat Technol, Shanghai, Peoples R China

[3] Univ Chinese Acad Sci, Beijing, Peoples R China

[4] ShanghaiTech Univ, Sch Informat Sci & Technol, Shanghai, Peoples R China

来源：

ADVANCES IN SPACE RESEARCH | 2018年 / 61卷 / 08期

关键词：

Autonomous navigation; Star sensor; Infrared horizon sensor; Installation error; Measurement error; Onboard data; NAVIGATION SATELLITES; ALGORITHM;

D O I：

10.1016/j.asr.2018.01.017

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper focuses on the autonomous orbit determination accuracy of Beidou MEO satellite using the onboard observations of the star sensors and infrared horizon sensor. A polynomial fitting method is proposed to calibrate the periodic error in the observation of the infrared horizon sensor, which will greatly influence the accuracy of autonomous orbit determination. Test results show that the periodic error can be eliminated using the polynomial fitting method. The User Range Error (URE) of Beidou MEO satellite is less than 2 km using the observations of the star sensors and infrared horizon sensor for autonomous orbit determination. The error of the Right Ascension of Ascending Node (RAAN) is less than 60 mu rad and the observations of star sensors can be used as a spatial basis for Beidou MEO navigation constellation. (C) 2018 COSPAR. Published by Elsevier Ltd. All rights reserved.

引用

页码：1975 / 1983

页数：9

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