Inertial-aided spacecraft angles-only navigation method based on adaptive square-root EKF

被引：0
|
作者：
Du, Ronghua [1 ]
Liao, Wenhe [1 ]
Zhang, Xiang [1 ]
机构：
[1] School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing,210094, China
来源：
Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology | 2022年 / 30卷 / 02期
关键词：
Covariance matrix - Extended Kalman filters - Navigation - Navigation systems - Observability - Simulation platform - Space rendezvous;
D O I：
10.13695/j.cnki.12-1222/o3.2022.02.011
中图分类号：
学科分类号：
摘要：
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页码：210 / 217
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