摘要
旋转捷联惯导系统采用旋转调制误差补偿技术对陀螺仪和加速度计误差进行调制,可以提高系统导航精度。文章借助捷联系统基本误差方程,简要分析了旋转调制误差补偿的机理;通过对几种典型IMU旋转方案的分析和仿真,验证了旋转调制误差补偿技术的有效性并比较了不同旋转方案的特点。
Rotating strapdown inertial navigation system （RINS） can modulate the gyro and accelerometer error with error rotating compensation method to improve the precision. The error model of the SINS and the mechanism of the error rotating compensation were analyzed in this paper. Based on analysis and simulation of several typical IMU rotating modulation schemes, the validity of the error rotating compensation technology was proved and the characteristic of the rotating schemes were compared
出处
《海军航空工程学院学报》
2012年第4期377-380,384,共5页
Journal of Naval Aeronautical and Astronautical University
关键词
捷联惯导
旋转调制
误差补偿
旋转方案
strapdown inertial navigation system （SINS）
rotating modulation
error compensation
rotating scheme
