An Unscented Kalman Filter–based iterative learning controller for multibody rotating scan optical spacecraft

被引：1

作者：

Zhao, Xian ^{[1
]}

Geng, Yunhai ^{[1
]}

Yuan, Chao ^{[2
]}

Wu, Baolin ^{[1
]}

机构：

[1] Research Center of Satellite Technology, Harbin Institute of Technology, China

[2] Shanghai Institute of Aerospace Technology, China

来源：

Transactions of the Institute of Measurement and Control | 2022年 / 44卷 / 12期

关键词：

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Backstepping - Degrees of freedom (mechanics) - Controllers - Kalman filters - Errors - Two term control systems

引用

页码：2418 / 2433

共 2 条

[1] Unscented Schmidt-Kalman filter on Lie groups with application to spacecraft attitude estimation
Zhu, Hangbiao
Gui, Haichao
Zhong, Rui
Advances in Space Research, 74 (11): : 5713 - 5724
[2] Combined tracking strategy based on unscented kalman filter for global positioning system L2C CM/D signal
Key Laboratory of Micro-Inertial Instrument and Advanced Navigation Technology of Ministry of Education, School of Instrument Science and Engineering, Southeast University, Nanjing
210 096, China
不详
212 013, China
Def. Sci. J., 5 (395-402):