Initial alignment of inertial navigation system based on fuzzy adaptive Kalman filter

被引：0
|
作者：
Wang, XL [1 ]
Shen, GX [1 ]
机构：
[1] Beijing Univ Aeronaut & Astronaut, Beijing 100083, Peoples R China
来源：
PROCEEDINGS OF THE SECOND INTERNATIONAL SYMPOSIUM ON INSTRUMENTATION SCIENCE AND TECHNOLOGY, VOL 3 | 2002年
关键词：
SINS; initial alignment; Kalman filter; fuzzy logic control;
D O I：
暂无
中图分类号：
O65 [分析化学];
学科分类号：
070302 ; 081704 ;
摘要：
A new initial of alignment of Strapdown inertial navigation system (SINS) based on the fuzzy Kalman filter is proposed. Fuzzy logic has been incorporated to tune the system error covariance of the filter in the initial alignment process. The simulation results have shown that the using of fuzzy Kalman filter for initial alignment can improve the consistency of the filter and the estimation accuracy. In the meantime the alignment time is reduced considerably.
引用
收藏
页码：887 / 891
页数：5
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