MEMS-based SINS/GNSS tightly-coupled navigation aided by time-differenced carrier-phase measurements

被引：0
|
作者：
Dong, Yi [1 ]
Wang, Dingjie [2 ]
Wu, Jie [2 ]
机构：
[1] State Key Laboratory of Astronautic Dynamics, Xi'an Satellite Control Center, Xi'an,710043, China
[2] College of Aerospace Science and Engineering, National University of Defense Technology, Changsha,410073, China
来源：
Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology | 2021年 / 29卷 / 04期
关键词：
Kalman filters;
D O I：
10.13695/j.cnki.12-1222/o3.2021.04.005
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：451 / 458
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