1·The inertial navigation technology includes platform inertial navigation system and SINS.
包括平台式惯导系统和捷联惯导系统。
2·The drift performance of IFOG must be improved in order to apply IFOG to inertial navigation.
为了把IFOG应用于惯性导航领域，必须改善其漂移特性。
3·The principle of equivalence is of critical importance in our analysis of inertial navigation.
等效原理在惯性导航分析中特别重要。
4·Strapdown inertial navigation technology has been widely used in military and national production.
捷联惯导技术在军事和国民生产诸多领域有着广泛的应用。
5·This area of study is central to the technology of inertial navigation and gyroscopic stabilization.
这个研究领域是惯性导航和陀螺稳定器技术的核心。
6·Linear and nonlinear error models for Inertial Navigation System (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。
7·This paper presents a new continuous self-calibration and alignment technology of inertial navigation platform.
提出了一种新的惯导误差系数标定方法———连续自标定自对准方法。
8·The results show that gravity disturbance vector is a major error source for high accuracy inertial navigation system.
结果表明，不确定的重力扰动向量是高精度惯导系统的一个重要误差源。
9·In this paper, the parameter identification technique of inertial navigation platform drifting error model is studied.
本文研究了惯导平台漂移误差模型的参数辨识技术。
10·The scale-factor error of inertia component is greatly influential to the precision of Inertial Navigation System (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。