1.The attitude solution for carrier is one of the key technologies for precision navigation of Strapdown Inertial Navigation System(SINS).
载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一。
2.Historically, normal gravity was satisfactory for free inertial navigation for the poor inertial sensor.
过去，由于惯性传感器精度较低，一般采用正常重力进行重力补偿已能够满足要求。
3.So the affection of temperature on these gyros is always the major research of inertial navigation.
温度对硅微陀螺仪性能的影响也一直是惯性导航研究的重点课题。
4.The simulation results indicate that the calibration can compensate the error and improve the precision of the inertial navigation system.
仿真结果表明，该标定方法能够对误差进行补偿，进而提高惯导系统的导航精度。
5.Avionics systems include a highly accurate inertial navigation system in which a computer provides steering information to the pilot.
航电系统包括高度精确的惯性导航系统，它通过电脑向飞行员提供转向信息。
6.Inertial navigation is a technology that utilize inertial components to measure aircraft's position, velocity, gesture and flight course.
惯性导航是利用惯性敏感器的测量信息来获得运载体位置、速度、姿态和航向的导航方法。
7.Main reasons for heading effect drift of an airborne platform inertial navigation system are analyzed in this paper.
本文分析了某型机载平台式惯性导航系统航向效应漂移产生的主要原因。
8.Inertial navigation system is composed of strap down inertial navigation system and platform inertial navigation system.
惯性导航定位系统分为平台式惯导系统和捷联式惯导系统两种。
9.An online identification algorithm of odometers scale factor in land used strapdown inertial navigation system is put forward.
提出陆用捷联惯导系统中里程计刻度因子的在线辨识算法。
10.In the paper, the scrolling compensation algorithm in position updating of strap down inertial navigation system is researched.
研究了高动态环境下捷联惯导位置更新中的涡卷补偿算法。