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Design and implementation of an Attitude and Heading Reference System (AHRS)

机译:航向参考系统(AHRS)的设计与实现

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This paper deals with the development and implementation of a cheap Micro Attitude and Heading Reference System (AHRS) using low-cost inertial and magnetic sensors. The orientation is parameterized with unit quaternion and the data fusion is done unifying a quaternion linear formulation of Wahba''s problem with a Multiplicative Extended Kalman Filter. It includes the gyro bias model. The estimation methodology proposed in this work is implemented and evaluated in real time, in order to assess its effectiveness. Special attention was paid to the low power consumption, speed and weight requirements, leading to the selection of a 16-bit microcontroller. The sensor suite is based on a tri-axis accelerometer, a dual axis gyro, a single axis gyro and a tri-axis magnetometer. Furthermore, the system is equipped with a Bluetooth module, which provides wireless capabilities. The total system supply voltage is 3.3 V. The dimension and weight are 60×40×15 mm and 60 g, respectively. The attitude rate estimation is 55.5 Hz.
机译:本文讨论了使用低成本惯性和磁传感器的廉价微型姿态和航向参考系统(AHRS)的开发和实现。使用单位四元数对方向进行参数化,并通过乘性扩展卡尔曼滤波器将Wahba问题的四元数线性表示统一起来,完成数据融合。它包括陀螺仪偏置模型。为了评估其有效性,本工作中提出的估算方法将得到实时实施和评估。特别关注低功耗,速度和重量要求,从而选择了16位微控制器。该传感器套件基于三轴加速度计,双轴陀螺仪,单轴陀螺仪和三轴磁力计。此外,系统配备了蓝牙模块,该模块提供无线功能。系统总电源电压为3.3V。尺寸和重量分别为60×40×15 mm和60 g。姿态速率估计为55.5 Hz。

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