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基于SINS速度信息的里程计参数快速标定方法

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针对里程计标度因数误差和安装误差对捷联惯导/里程计组合导航精度的显著影响,提出一种基于短时捷联惯导系统(strapdown inertial navigation system,SINS)速度信息的里程计参数标定方法.通过建立航位推算误差模型,构建惯性测量单元(inertial measurement unit,IMU)坐标系内惯导系统输出速度与里程计输出之间的关系式,得到里程计参数的计算公式;利用最小二乘法对里程计标度因数和安装误差进行标定.该方法只利用了捷联惯导信息,在 1 min内就可实现里程计参数的初次标定,不需要相关参数误差值为小量的假设,并可以忽略杆臂效应对标定效果的影响.试验结果表明:当车辆行驶 30 min后,利用该方法标定后的水平航位推算精度比传统标定方法定位精度高92.3%.
Fast Calibration Method of Odometer Parameters Based on Speed Information of Strapdown Inertial Navigation System
To solve the problem that the scale factor error and installation error of odometers have a great influence on the accuracy of strapdown inertial navigation/odometer integrated navigation,a fast calibration method based on short-term SINS(strapdown inertial navigation system)information is proposed for odometer parameters.By establishing a dead-reckoning error model,the relationship between the output speed of the inertial navigation system and the output of the odometer in the inertial measurement unit(IMU)coordinate system is constructed,and the formula of calculating the odometer parameters is obtained.The least squares method is utilized to calibrate the odometer scale factor and installation error.This method only uses strap-down inertial navigation information to achieve the initial calibration of the odometer parameters within 1 min.It does not require the assumption that the error value of the relevant parameters is small,and ignores the influence of the lever arm effect on the calibration effect.The test results show that,when the vehicle has been running for 30 min,the accuracy of the horizontal dead-reckoning method calibrated by this method is 92.3%higher than that of the traditional calibration method.

odometerscale factorinstallation errorSINSleast squares method

周召发、梁哲、徐志浩、常振军、陈河、赵芝谦

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火箭军工程大学导弹工程学院,陕西西安 710025

火箭军研究院,北京 100094

车辆里程计 标度因数 安装误差 捷联惯导 最小二乘

航空科学基金

201808U8004

2024

西南交通大学学报
西南交通大学

西南交通大学学报

CSTPCD北大核心
影响因子:0.973
ISSN:0258-2724
年,卷(期):2024.59(2)
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