Yuan Xuebing, Yu Shuai, Zhang Shengzhi, Wang Guoping, Liu Sheng
School of Mechanical Science and Engineering, Huazhong University of Science and Technology, 1037 Luoyu Road, Wuhan 430074, China.
School of Power and Mechanical Engineering, Wuhan University, 8 East Lake South Road, Wuhan 430072, China.
Sensors (Basel). 2015 May 7;15(5):10872-90. doi: 10.3390/s150510872.
Inertial navigation based on micro-electromechanical system (MEMS) inertial measurement units (IMUs) has attracted numerous researchers due to its high reliability and independence. The heading estimation, as one of the most important parts of inertial navigation, has been a research focus in this field. Heading estimation using magnetometers is perturbed by magnetic disturbances, such as indoor concrete structures and electronic equipment. The MEMS gyroscope is also used for heading estimation. However, the accuracy of gyroscope is unreliable with time. In this paper, a wearable multi-sensor system has been designed to obtain the high-accuracy indoor heading estimation, according to a quaternion-based unscented Kalman filter (UKF) algorithm. The proposed multi-sensor system including one three-axis accelerometer, three single-axis gyroscopes, one three-axis magnetometer and one microprocessor minimizes the size and cost. The wearable multi-sensor system was fixed on waist of pedestrian and the quadrotor unmanned aerial vehicle (UAV) for heading estimation experiments in our college building. The results show that the mean heading estimation errors are less 10° and 5° to multi-sensor system fixed on waist of pedestrian and the quadrotor UAV, respectively, compared to the reference path.
基于微机电系统(MEMS)惯性测量单元(IMU)的惯性导航因其高可靠性和独立性吸引了众多研究人员。航向估计作为惯性导航最重要的部分之一,一直是该领域的研究热点。使用磁力计进行航向估计会受到诸如室内混凝土结构和电子设备等磁干扰的影响。MEMS陀螺仪也用于航向估计。然而,陀螺仪的精度会随时间变得不可靠。本文根据基于四元数的无迹卡尔曼滤波器(UKF)算法,设计了一种可穿戴多传感器系统,以获得高精度的室内航向估计。所提出的多传感器系统包括一个三轴加速度计、三个单轴陀螺仪、一个三轴磁力计和一个微处理器,将尺寸和成本降至最低。该可穿戴多传感器系统固定在行人腰部以及四旋翼无人机(UAV)上,在我校建筑中进行航向估计实验。结果表明,与参考路径相比,固定在行人腰部和四旋翼无人机上的多传感器系统的平均航向估计误差分别小于10°和5°。