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·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。
3·The design of gyroscope data acquisition system for Marine strapdown inertial navigation system is presented.
介绍了船用捷联惯性导航系统中陀螺仪数据采集系统的设计。
4·A new type of inertial navigation system combining customary platform type with strap-down one is put forward.
本文提出一种把平台式和捷联式惯导系统结合在一起的新的惯性导航系统。
5·Main reasons for heading effect drift of an airborne platform inertial navigation system are analyzed in this paper.
文中分析了某型平台式惯性导航系统航向漂移产生的主要原因。
6·Inertial navigation system (INS) is a important navigation system with widely application in civil and military field.
惯性导航系统(INS)是一种非常重要的导航定位系统，在民用和军事领域有广泛的应用。
7·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。
8·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。
9·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。
10·Compared with Platform Inertial Navigation System, SINS is smaller in size, lighter in weight, more reliable and cheaper.
它与平台式惯性导航系统相比具有体积小、重量轻、成本低、可靠性高等诸多优点。