strapdown inertial navigation system 捷联式惯性导航系统 ; 捷联式惯导系统 ; 惯性导航系统 ; 捷联惯导系统
Inertial Navigation System INS 惯性导航系统
inertial navigation system ih 惯导系统
ship inertial navigation system 船舶惯导
INS Inertial Navigation System 惯性导航系统
Loran-inertial navigation system 罗兰
laser inertial navigation system 激光惯性导航系统
double inertial navigation system 双惯导系统
Loran inertial navigation system 劳兰惯性导航系统
At first, some kinds of coordinate in the inertial navigation system are defined. Then, the attitude update algorithms of SIS are studied, and the basic dynamics equations based on geography coordinate are introduced.
首先定义了几种导航常用坐标系,阐述了捷联惯性系统的基本工作原理,然后研究了捷联惯性系统的姿态更新算法,进而基于地理坐标系给出其基本动力学方程,并推导了误差方程。
参考来源 - 捷联惯性系统初始对准研究·2,447,543篇论文数据，部分数据来源于NoteExpress
以上来源于: WordNet
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。
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。
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。
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