Linear and nonlinear error models for InertialNavigationSystem (INS) initial alignment are established.
建立了惯导系统(INS)初始对准的线性和非线性误差模型。
2
The scale-factor error of inertia component is greatly influential to the precision of InertialNavigationSystem (INS).
在惯性导航系统中，惯性元件的标度因数误差对系统的误差产生了极大的影响。
3
There exists a slope drift in an integral gyro when it is used as an azimuth gyro, which may cause serious heading and position errors in the InertialNavigationSystem (INS).