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Attitude Heading Estimation of Indoor Moving Object Based on Extended Kalman Filter Algorithm

机译:基于扩展卡尔曼滤波算法的室内运动物体姿态航向估计

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Inertial navigation based on Micro-Electro-Mechanical System (MEMS) sensors has recently received much attention. Attitude heading estimation of an indoor moving object, as one of the important parts of inertial navigation is still worth studying. Attitude heading estimation using the acceleration and magnetic sensors fixed on the indoor moving object can easily be disturbed by surrounding environments or other factors. The gyroscope can also be used for computing the attitude heading. However, due to its own characteristics that the estimated errors gradually accumulates, the accuracy is not reliable for a long time. In this paper, quaternion-based Extended Kalman Filter algorithm is proposed to estimate the attitude heading of indoor moving object combining the acceleration sensor, magnetic sensor and gyroscope. For the method, the quaternion derived from gyroscope's readings is selected as the state vector of the filter, and the quaternion calculated from the measurements of accelerometer and magnetometer is used for the observations of the filter. The real-time estimated results are achieved by the state update of the designed filter. The experiment result shows that the proposed method can effectively improve the accuracy of the attitude heading estimation, compared with the complementary filtering.
机译:基于微机电系统(MEMS)传感器的惯性导航最近受到了广泛关注。作为惯性导航的重要组成部分之一,室内运动物体的姿态航向估计仍然值得研究。使用固定在室内移动物体上的加速度和磁传感器进行的姿态航向估计很容易受到周围环境或其他因素的干扰。陀螺仪也可以用于计算姿态航向。但是,由于估计误差逐渐累积的自身特性,因此精度长期以来并不可靠。提出了一种基于四元数的扩展卡尔曼滤波算法,结合加速度传感器,磁传感器和陀螺仪来估计室内运动物体的姿态航向。对于该方法,选择从陀螺仪读数得出的四元数作为滤波器的状态向量,并根据加速度计和磁力计的测量结果计算出的四元数用于滤波器的观测。实时估计结果是通过设计滤波器的状态更新获得的。实验结果表明,与补充滤波相比,该方法可以有效提高姿态航向估计的准确性。

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