Determination of time delays in measurement channels during SINS calibration in inertial mode

被引：5
作者：
Klimkovich B.V. [1 ]
Tolochko A.M. [1 ]
机构：
[1] OKB TSP, Minsk
来源：
Gyroscopy and Navigation | 2016年 / 7卷 / 2期
关键词：
Kalman Filter; Dynamic Test; Velocity Error; Rate Table; Strapdown Inertial Navigation System;
D O I：
10.1134/S2075108716020048
中图分类号：
学科分类号：
摘要：
The article presents a method of determining gyro and accelerometer delays during calibration of strapdown inertial navigation systems (SINS) of navigation accuracy. The method uses the Kalman filter in SINS navigation mode and estimates errors in gyro and accelerometer delays and scale factors, sensitivity axes misalignment and drift, coordinates of accelerometer proof masses in the body-fixed frame. Application of SINS navigation mode during calibration reduces the requirements to accuracy of the rate table. The obtained estimates of calibration parameters are self-consistent, minimizing the resulting SINS error. The method was tested during calibration of FOG-based SINS. © 2016, Pleiades Publishing, Ltd.
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页码：137 / 144
页数：7
相关论文
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