Journal of Projectiles, Rockets, Missiles and Guidance >
Algorithm for MTI-based Integrated Navigation
Received date: 2009-09-02
Online published: 2025-05-28
A kind of MR/DR navigation mode was deduced. An accelerometer and a magnetometer were used for calculating the carrier's attitude angle for correcting the carrier's attitude angle calculated by the gyro. The application of robust self-tuning Kalman filter in GPS/SINS system was discussed. The simulation results show that the robust self-tuning Kalman filter's filtering effect is superior to that of the standard Kalman filter.
Key words： MR/DR; GPS/SINS; Kalman filter; robust self-tuning
JI Zhenlong , QIAN Feng . Algorithm for MTI-based Integrated Navigation[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(4) : 11 -14 . DOI: 10.15892/j.cnki.djzdxb.2010.04.041
| [1] | 黄卫权, 董冀. 基于MTi 微惯性航姿系统的卡尔曼滤波器设计[J]. 通信与信息处理, 2009, 28(1): 54-57. |
| [2] | 袁信, 俞济祥, 陈哲. 导航系统[M]. 北京: 航空工业出版社, 1993: 175-186. |
| [3] | 高为广, 杨元喜, 张双成. 基于当前加速度模型的抗差自适应卡尔曼滤波[J]. 测绘学报, 2006, 35(1): 15-18. |
| [4] | 耿延睿, 崔中兴. 组合导航系统卡尔曼滤波衰减因子自适应估计算法研究[J]. 中国惯性技术学报, 2001, 9(4): 8-10. |
/
| 〈 |
|
〉 |