应用无线电近导系统测量的距离和方位校正惯导是一种新的综合导航方式。
It is new mode in integrated navigation that INS is corrected with distance and orientation measured by wireless navigation system.
文中基于准三维模型对惯导系统误差校正的思想，利用摄像机成像系统和捷联惯导系统（SINS）相结合的方法，着重对量测矩阵进行推导。
Based on the INS error correction by quasi-three dimensional model, the method of the combination of camera imaging system with SINS to deduce the measurement matrix was utilized.
利用里程仪可以抑制惯导的误差积累，但里程仪刻度系数误差对组合系统的定位精度影响很大，必须对其进行校正。
The error accumulation of inertial navigation system can be restrained via OD, however, OD scale factor error has remarkable effect on the positioning precision.
从校正方式组成及原理入手，详细地介绍了某型飞机导航系统惯导几种校正方式的使用特点及相互交联关系。
Theory, operating features and interface relations of three correction modes for the inertial navigation; Short-Range Radio Navigation, Long-Range Radio Navigation and Visual, are presented.
针对用机载雷达校正飞机惯导系统的方案，研究为满足校正精度应对雷达性能指标提出的要求。
With regard to the scheme of inertial navigation system correction with airborne radar, this paper studies the radar performance requirement in order to meet the correction precision.
针对用机载雷达校正飞机惯导系统的方案，研究为满足校正精度应对雷达性能指标提出的要求。
With regard to the scheme of inertial navigation system correction with airborne radar, this paper studies the radar performance requirement in order to meet the correction precision.
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