A Novel Approach to Calculating Yaw Angles Using an Accelerometer Sensor

A. Nurhakim, M. R. Effendi, H. Saputra, Rina Mardiati, T. Priatna, N. Ismail
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引用次数: 1

Abstract

An accelerometer can be used to calculate pitch and roll orientation angles. However, the accelerometer sensor cannot calculate the yaw angle, so a novel approach is needed to calculate the yaw angle. This research focuses on designing a new algorithm for calculating yaw orientation angles using an accelerometer sensor. Tests are carried out using the Stewart Platform which is moved rotating on the yaw axis clockwise. The measurement results show that the calculation of the yaw orientation angle using the accelerometer sensor has an average percentage error of 6.42% with the biggest error value at the parameter angle of 60° and the smallest value at the parameter angle of 10°. Based on the measurement of standard deviation, the most precise value at the parameter angle of 30° and the least precise value at parameter angle of 50°. The average standard deviation is 0.45°. The standard deviation value shows that this method has a fairly good precision level so that it is worthy of being used as an alternative measure of yaw angle.
一种利用加速度计传感器计算偏航角的新方法
加速度计可以用来计算俯仰角和横摇角。然而,由于加速度计传感器无法计算横摆角,因此需要一种新的方法来计算横摆角。本研究的重点是设计一种利用加速度计传感器计算偏航方向角的新算法。试验采用沿偏航轴顺时针旋转的Stewart平台进行。测量结果表明,利用加速度计传感器计算偏航定向角的平均百分比误差为6.42%,在参数角为60°时误差最大,参数角为10°时误差最小。根据标准偏差的测量,参数角为30°时最精确,参数角为50°时最不精确。平均标准差为0.45°。标准差值表明,该方法具有较好的精度水平,值得作为偏航角的替代测量方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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