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速率偏频激光惯性测量单元航向效应补偿方法研究

Study on the method of compensation for the heading effect of the rate offset frequency laser inertial measurement unit.

作者信息

Xu Binghua, Zhu Zhanxia, Yuan Yichao, Jiang Yifu, Yuan Jianping

出版信息

Appl Opt. 2019 Dec 10;58(35):9634-9642. doi: 10.1364/AO.58.009634.

DOI:10.1364/AO.58.009634
PMID:31873563
Abstract

For the rate offset frequency laser inertial measurement unit (IMU), the errors of its three attitude angles, laser gyroscope, and accelerometer are coupled, which will affect the initial alignment result of the IMU and will make the measurement results of the IMU at different positions and angles deviate from the truth value. Meanwhile, with the increase of tilt angle, the heading effect becomes more obvious, and the error value is distributed positively cosine with the heading angle. In order to ensure the adaptability of the IMU to various operating conditions, it is necessary to compensate for the heading effect. The contribution of each error source of IMU to the heading effect is theoretically studied in this paper. We present a new method for compensating for the heading effect of the rate offset frequency laser IMU, in which the normal drift error of the vertical direction laser gyroscope and the zero bias error of the accelerometer under the turntable coordinate system are compensated. Based on the above method, simulation analysis and test verification are carried out. The experimental results show that the compensation method has a remarkable effect. In the case of two horizontal attitude angles tilted 0.0873 rad and 5 min initial alignment, the error of the rate offset frequency laser IMU reduced from 5.02E-04 rad $({3}\sigma)$(3σ) to 1.45E-04 rad $({3}\sigma)$(3σ), and the accuracy increased by 71%. High-precision initial alignment is achieved, which can meet the requirements of high-precision engineering applications.

摘要

对于速率偏频激光惯性测量单元(IMU),其三个姿态角、激光陀螺和加速度计的误差相互耦合,这会影响IMU的初始对准结果,导致IMU在不同位置和角度的测量结果偏离真值。同时,随着倾斜角的增大,航向效应变得更加明显,误差值与航向角呈正余弦分布。为确保IMU对各种工作条件的适应性,有必要对航向效应进行补偿。本文从理论上研究了IMU各误差源对航向效应的贡献。提出了一种速率偏频激光IMU航向效应补偿新方法,该方法对转台坐标系下垂直方向激光陀螺的常值漂移误差和加速度计的零偏误差进行补偿。基于上述方法进行了仿真分析和试验验证。实验结果表明,该补偿方法效果显著。在两个水平姿态角倾斜0.0873 rad且初始对准为5 min的情况下,速率偏频激光IMU的误差从5.02E-04 rad(3σ)降至1.45E-04 rad(3σ),精度提高了71%。实现了高精度初始对准,能够满足高精度工程应用的要求。

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