Improved Multi-Position Calibration Method for Mechanical Inertia Measurement Units

Salem Abd El-Hakem Hegazy, A. Kamel, I. Arafa, Y. Elhalwagy
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引用次数: 2

Abstract

Inertial Navigation System (INS) is used in a variety of applications such as missile and marine navigation. INS is comprised of an inertial measuring unit (IMU) and a processor unit that performs the navigation mathematics calculations. In order to get accurate navigation data via INS, calibration of IMU sensors are necessary. Mechanical sensors are used in high-precision navigation, such as strategic missiles and are characterized by their low random noise. However, deterministic errors can cause very significant errors in positioning such as biases, scale factors, non-orthogonality errors, and g-sensitive and non-g-sensitive drifts. Therefore, determining an effective and accurate method of calibration is necessary to estimate and compensate for these errors. The suggested methodology accurately calculates the calibration parameters to minimize those errors. The traditional calibration techniques of the accelerometer are restricted in precision, since the estimation of scale factor and bias obtained from a limited number of positions depending on the gravity direction. These calibration techniques are also limited in the estimation of g-sensitive and non-g-sensitive drifts impacting gyro performance. This paper presents a new technique of calibration that overcomes these drawbacks, based on an enhancement of multi-position technique. Experimental results for the proposed technique was carried out to confirm its efficiency.
改进的机械惯性测量单元多位置标定方法
惯性导航系统(INS)用于导弹和船舶导航等多种应用。INS由惯性测量单元(IMU)和执行导航数学计算的处理器单元组成。为了通过惯导系统获得准确的导航数据,必须对惯导单元传感器进行标定。机械传感器用于高精度导航,如战略导弹,具有低随机噪声的特点。然而,确定性误差会导致非常显著的定位误差,如偏差、尺度因子、非正交性误差以及g敏感和非g敏感漂移。因此,确定一种有效和准确的校准方法是必要的,以估计和补偿这些误差。建议的方法准确地计算校准参数,以尽量减少这些误差。传统的加速度计标定技术由于在有限的位置上得到的尺度因子和偏差的估计依赖于重力方向,其精度受到限制。这些校准技术在估计g敏感和非g敏感漂移影响陀螺性能方面也受到限制。本文在多位置标定技术的基础上提出了一种新的标定技术,克服了这些缺点。实验结果验证了该方法的有效性。
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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