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Enhanced Pedestrian Navigation Based on Course Angle Error Estimation Using Cascaded Kalman Filters

机译:基于级联卡尔曼滤波的航向角误差估计的增强型行人导航

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An enhanced pedestrian dead reckoning (PDR) based navigation algorithm, which uses two cascaded Kalman filters (TCKF) for the estimation of course angle and navigation errors, is proposed. The proposed algorithm uses a foot-mounted inertial measurement unit (IMU), waist-mounted magnetic sensors, and a zero velocity update (ZUPT) based inertial navigation technique with TCKF. The first stage filter estimates the course angle error of a human, which is closely related to the heading error of the IMU. In order to obtain the course measurements, the filter uses magnetic sensors and a position-trace based course angle. For preventing magnetic disturbance from contaminating the estimation, the magnetic sensors are attached to the waistband. Because the course angle error is mainly due to the heading error of the IMU, and the characteristic error of the heading angle is highly dependent on that of the course angle, the estimated course angle error is used as a measurement for estimating the heading error in the second stage filter. At the second stage, an inertial navigation system-extended Kalman filter-ZUPT (INS-EKF-ZUPT) method is adopted. As the heading error is estimated directly by using course-angle error measurements, the estimation accuracy for the heading and yaw gyro bias can be enhanced, compared with the ZUPT-only case, which eventually enhances the position accuracy more efficiently. The performance enhancements are verified via experiments, and the way-point position error for the proposed method is compared with those for the ZUPT-only case and with other cases that use ZUPT and various types of magnetic heading measurements. The results show that the position errors are reduced by a maximum of 90% compared with the conventional ZUPT based PDR algorithms.
机译:提出了一种改进的基于行人航位推算(PDR)的导航算法,该算法使用两个级联的卡尔曼滤波器(TCKF)来估计航向角和导航误差。所提出的算法使用了安装在脚上的惯性测量单元(IMU),安装在腰部的磁传感器以及基于零速度更新(ZUPT)的带有TCKF的惯性导航技术。第一级滤波器估计人的航向角误差,该误差与IMU的航向误差密切相关。为了获得航向测量值,滤波器使用了磁传感器和基于位置轨迹的航向角。为了防止磁干扰污染估算,将磁传感器连接到腰带。由于航向角误差主要是由于IMU的航向误差引起的,并且航向角的特性误差高度依赖于航向角的特性误差,因此估算的航向角误差用作估计航向误差的度量。第二阶段过滤器。在第二阶段,采用了惯性导航系统扩展的卡尔曼滤波器-ZUPT(INS-EKF-ZUPT)方法。由于航向误差是通过使用航向角误差测量直接估算的,因此与仅使用ZUPT的情况相比,航向和偏航陀螺仪偏置的估算精度可以提高,最终可以更有效地提高位置精度。通过实验验证了性能的增强,并将该方法的航点位置误差与仅ZUPT的情况以及使用ZUPT和各种类型的磁航向测量的其他情况进行了比较。结果表明,与传统的基于ZUPT的PDR算法相比,位置误差最多可减少90%。

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