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GNSS autonomous navigation method for HEO spacecraft

Yuan Dehu Sun Jun Han Fei Chen Yang Chen Yun

高技术通讯（英文版）2020，Vol.26Issue(2)：188-195,8.

高技术通讯（英文版）2020，Vol.26Issue(2)：188-195,8.DOI:10.3772/j.issn.1006-6748.2020.02.008

GNSS autonomous navigation method for HEO spacecraft

Yuan Dehu ¹Sun Jun ²Han Fei ¹Chen Yang ²Chen Yun¹

作者信息

1. Shanghai Aerospace Control Technology Institute,Shanghai 201109,P.R.China
2. Shanghai Key Laboratory of Space Intelligent Control Technology,Shanghai 201109,P.R.China
折叠

摘要

关键词

global navigation satellite system ( GNSS)/high earth orbit ( HEO)/chaotic os-cillator/autonomous navigation

Key words

global navigation satellite system ( GNSS)/high earth orbit ( HEO)/chaotic os-cillator/autonomous navigation

引用本文复制引用

Yuan Dehu,Sun Jun,Han Fei,Chen Yang,Chen Yun..GNSS autonomous navigation method for HEO spacecraft[J].高技术通讯（英文版）,2020,26(2):188-195,8.

基金项目

Supported by the National Key Research and Development Program of China(No.2016YFB0501000),the Major Program of National Natural Science Foundation of China(No.61690214)and the Project of D020214. （No.2016YFB0501000）

高技术通讯（英文版）

OAEI

ISSN：1006-6748

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