Attitude determination for satellite using adaptive unscented Kalman filter

被引：0
|
作者：
Xiao, Lei [1 ,2 ,3 ]
Wang, Shao-Ju [1 ,3 ]
Chang, Lin [1 ,3 ]
Zhou, Mei-Li [1 ,3 ]
机构：
[1] Changchun Institute of Optics, Fine Mechanics& Physics, Chinese Academy of Sciences, Changchun,130033, China
[2] University of Chinese Academy of Sciences, Beijing,100049, China
[3] Key Laboratory of Space-based Dynamic & Rapid Optical Imaging Technology, Chinese Academy of Sciences, Changchun,130033, China
来源：
Guangxue Jingmi Gongcheng/Optics and Precision Engineering | 2021年 / 29卷 / 03期
关键词：
Compendex;
D O I：
10.37188/OPE.20212903.0637
中图分类号：
学科分类号：
摘要：
Kalman filters - Satellites - Covariance matrix - Adaptive filters - Errors
引用
收藏
页码：637 / 645
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