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基于组合导航技术的光纤捷联系统在线标定
引用本文:张小跃,张春熹,宋凝芳.基于组合导航技术的光纤捷联系统在线标定[J].航空学报,2008,29(6):1656-1659.
作者姓名:张小跃  张春熹  宋凝芳
作者单位:北京航空航天大学仪器科学与光电工程学院,北京,100191
摘    要: 将光纤捷联系统惯性测量单元(IMU)输出误差分解成零偏误差、标度因数误差、失准角误差和随机白噪声几个部分,建立了系统误差模型,基于此模型设计卡尔曼滤波器引入高精度外部信息源对IMU进行在线标定。将此方法应用于某光纤捷联系统进行跑车试验,结果表明:引入外部信息源进行在线标定与补偿后系统纯惯导精度显著提高,本文建立的系统误差模型和在线估计方式有效估计了IMU输出误差,实现了系统在线标定,提高了系统实用精度。

关 键 词:光纤陀螺  误差模型  卡尔曼滤波  在线估计  在线标定  

Online Calibration of FOG Strapdown System Based on Integrated Navigation Technology
Zhang Xiaoyue,Zhang Chunxi,Song Ningfang.Online Calibration of FOG Strapdown System Based on Integrated Navigation Technology[J].Acta Aeronautica et Astronautica Sinica,2008,29(6):1656-1659.
Authors:Zhang Xiaoyue  Zhang Chunxi  Song Ningfang
Institution:Zhang Xiaoyue,Zhang Chunxi,Song Ningfang (School of Instrument Science , Opto-electronic Engineering,Beijing University of Aeronautics , Astronautics,Beijing 100191,China)
Abstract:The output error of an inertial measurement unit(IMU) in a fiber optic gyro(FOG) strapdown inertial navigation system is divided into bias,scale factor,misalignment and white noise. A system error model is built,and a Kalman filter is designed fusing high precision information to calibrate the IMU online. This is applied into an FOG strapdown system and tested in a vehicle. The test results indicate that the free inertial navigation performance is greatly improved with the online calibration technique. The ...
Keywords:FOG  error model  Kalman filter  online estimation  online calibration  
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