Performance Improvement of Inertial Navigation System by Using Magnetometer with Vehicle Dynamic Constraints

被引:19
|
作者
Won, Daehee [1 ]
Ahn, Jongsun [2 ]
Sung, Sangkyung [2 ]
Heo, Moonbeom [3 ]
Im, Sung-Hyuck [3 ]
Lee, Young Jae [2 ]
机构
[1] Univ Colorado, Dept Aerosp Engn Sci, Boulder, CO 80309 USA
[2] Konkuk Univ, Dept Aerosp Informat Engn, Seoul 143701, South Korea
[3] Korea Aerosp Res Inst, Div Satellite Nav, Taejon 305806, South Korea
关键词
CALIBRATION;
D O I
10.1155/2015/435062
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
A navigation algorithm is proposed to increase the inertial navigation performance of a ground vehicle using magnetic measurements and dynamic constraints. The navigation solutions are estimated based on inertial measurements such as acceleration and angular velocity measurements. To improve the inertial navigation performance, a three-axis magnetometer is used to provide the heading angle, and nonholonomic constraints (NHCs) are introduced to increase the correlation between the velocity and the attitude equation. The NHCs provide a velocity feedback to the attitude, which makes the navigation solution more robust. Additionally, an acceleration-based roll and pitch estimation is applied to decrease the drift when the acceleration is within certain boundaries. The magnetometer and NHCs are combined with an extended Kalman filter. An experimental test was conducted to verify the proposed method, and a comprehensive analysis of the performance in terms of the position, velocity, and attitude showed that the navigation performance could be improved by using the magnetometer and NHCs. Moreover, the proposed method could improve the estimation performance for the position, velocity, and attitude without any additional hardware except an inertial sensor and magnetometer. Therefore, this method would be effective for ground vehicles, indoor navigation, mobile robots, vehicle navigation in urban canyons, or navigation in any global navigation satellite system-denied environment.
引用
收藏
页数:11
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