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Real-time and High-performance Attitude and Heading Reference System Based on MIMU/magnetometers

机译:基于MIMU /磁力计的实时和高性能姿态和前置参考系统

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In the paper, an attitude and heading reference system based on MIMU/magnetometers with moderate accuracy is presented. To meet the requirements of the real-time measurement, a master/slave CPU structure is proposed in order to improve the data refresh rate effectively. In the algorithm part, an adaptive extended Kalman filter equation is applied in the system, where the filter equation uses three tilt angles of attitude and three bias errors for the gyroscopes as state vectors, the measurements of three accelerometers and magnetometers are used to drive the state update. When the system is in dynamic mode, the measured values of the accelerometers consist of the gravity vector and the dynamic accelerations, an adaptive extended Kalman filter tunes its gain automatically based on the system dynamics sensed by the accelerometers to yield optimal performance. The experiment result shows that the attitude and heading angle errors are within 0.2 deg and 0.5 deg respectively in stationary mode, and the result can reflect the attitude angles reasonably in dynamic mode.
机译:在本文中,提出了一种基于具有中等精度的MIMU /磁力计的姿态和标题参考系统。为了满足实时测量的要求,提出了主/从CPU结构,以有效地提高数据刷新率。在算法部分中,在系统中应用自适应扩展卡尔曼滤波器方程,其中滤波器方程使用三个倾斜的姿态角度,以及陀螺仪作为状态向量的三个偏置误差,三个加速度计和磁力计的测量用于驱动状态更新。当系统处于动态模式时,加速度计的测量值由重力矢量和动态加速度组成,自适应扩展卡尔曼滤波器基于加速度计感测的系统动态自动调整其增益,以产生最佳性能。实验结果表明,姿态和标题角误差分别以固定模式分别在0.2°和0.5°内,结果可以在动态模式下合理地反映姿态角度。

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