Aircraft attitude estimation using an error state Kalman filter in the navigation coordinate system

被引：0
|
作者：
He, Lei [1 ,2 ]
Xuan, Xiaogang [3 ]
Luo, Xiaohu [3 ]
Jia, Bin [1 ,2 ]
Yang, Yibiao [1 ,2 ]
机构：
[1] Key Laboratory of the Ministry of Education for New Sensor and Intelligent Control, Taiyuan University of Technology, Taiyuan,030024, China
[2] College of Electronic Information And Optical Engineering, Taiyuan University of Technology, Taiyuan,030024, China
[3] Taiyuan Aviation Instrument Co, Ltd, 030032, China
来源：
Yi Qi Yi Biao Xue Bao/Chinese Journal of Scientific Instrument | 2024年 / 45卷 / 10期
关键词：
D O I：
10.19650/j.cnki.cjsi.J2412772
中图分类号：
学科分类号：
摘要：
22
引用
收藏
页码：295 / 304
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