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。
Abstract : A method to realize attitude algorithm module in strapdown inertial guidance is presented.
摘要 ：提出了捷联惯性导航系统姿态解算模块的一种实现方法。
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。
Attitude matrix is represented by quaternion and the calculation of attitude matrix is a key in Strapdown INS.
在捷联惯导系统中，可以用四元数来表示姿态矩阵，而姿态矩阵的计算是捷联惯导系统的关键问题之一。
On Improving Strapdown Inertial Navigation System(SINS) with Velocity Information of Active Radar Seeker (ARS);
主动雷达导引头可提供精确且稳定的测速信息，具有辅助惯导的潜力。
Strapdown Inertial Navigation System SINS-500 is based on Optolink's TRS-500 FOGs, precise accelerometers and board computer.
捷连惯性导航系统SINS- 500是基于TRS - 500的光纤陀螺仪、精密加速度传感器以及板式集散地。
An online identification algorithm of odometer's 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。
Strapdown Inertial Navigation System SINS-1000 is based on Optolink's SRS-1000 FOGs, precise accelerometers and board computer.
捷连惯性导航系统SINS- 1000是基于SRS - 1000的光纤陀螺仪、精密加速度传感器以及板式集散地。
A simple and utility field fast calibration method for the gyroflex strapdown inertial system has been presented in this paper .
本文给出了捷联式惯性导航系统一种简单实用的场地标定方法。
Quaternion method, which has been successfully applied to the Strapdown Inertial Navigation and Guidance for tens year, is classical.
数十年来，四元数及其解法成功地应用于捷联惯性导航和制导系统中，成为经典的算法。
Optolink's fiber-optic strapdown inertial navigation systems have complete solid-state design with no rotating or other moving parts.
该捷连系统为全固体设计，没有移动部件，适用于各种空中，陆地，水下设备。
The paper introduces a very low cost strapdown inertial guidance system consisting of piezoelectric gyros and low cost accelerometers.
提出一种低成本捷联惯性制导系统方案。该系统主要由压电陀螺和低成本加速度计构成。
A new approach to transfer alignment for the initial alignment of Strapdown inertial navigation systems on moving base was put forward.
针对捷联惯导系统的动基座初始对准问题，提出了一种新的动基座快速传递对准方案。
It is an effective way in integrated navigation by using Strapdown Inertial navigation System (SINS), GPS and Doppler Velocity Log (DVL).
利用捷联惯导(SINS)、GPS定位系统和多普勒计程仪(DVL)进行组合导航是水下运载器导航定位的有效方式。
In this paper, based on the inertial navigation equation, a novel model for the laser gyro strapdown inertial navigation system is provided.
本文从惯性导航基本方程出发，推导了激光陀螺捷联式惯性导航系统的系统级标定的一种误差标定模型。
At appraising the reliability of the missile-borne strapdown inertial navigation system, the reliability information for the key groups are needed.
在评价弹用捷联惯导系统的可靠性时，需要其关键件的可靠性信息。
Single gyro strapdown inertial navigation system (SGSINS) has many advantages, for example, small volume, light weight, low cost, high reliability and so on.
单陀螺捷联惯导系统（SGSINS）不仅具有和经典捷联惯导系统相同的基本功能，而且有体积小、重量轻、成本低、可靠性高等优点。
Base on wavelet denoising theory as well as the characteristic of the signal, a wavelet denoising method applied to Strapdown north seeking system was proposed.
文章基于小波变换的消噪原理，结合待测信号的特点，创造性地提出一种适用于捷联寻北仪的小波消噪法。
According to the feature of GALILEO system, this paper focuses on the GALILEO/Strapdown Inertial Navigation System (SINS)pseudo range integrated navigation mode.
GALILEO是新一代的全球卫星定位系统。文章根据GALILEO系统的特点，有针对性地研究了GALILEO/捷联惯导（SINS）伪距组合导航模式。
So-called GFSINS (gyroscope free strapdown inertial navigation system) is a kind of strapdown inertial navigation system with only accelerometers but no gyroscope.
无陀螺捷联惯导系统就是惯性元件只用加速度计，而不用陀螺的惯导系统。
During a transfer alignment of strapdown inertial navigation system, Kalman filter models are linear time varying system whose analysis of observability is difficult.
捷联惯导系统的卡尔曼滤波模型在传递对准时，为线性时变系统，而线性时变系统的可观测性分析比较困难。
The main navigation algorithm of strapdown inertial navigation system has been introduced, and the basic principles of strapdown inertial navigation system has been revealed.
对目前主要的捷联惯性导航系统解算方法进行介绍并对捷联惯性导航系统的基本原理进行分析。
Using astronavigation theory, the algorithm of calibrating the constant gyro drifts of ESG strapdown inertial navigation system and carrier heading is presented in this paper.
本文应用天文导航理论，根据GPS提供的位置信息，对静电陀螺捷联导航系统陀螺常值漂移和载体航向角进行校正的算法进行了研究。
The paper introduces a new experience platform which is based on the combination of the augmented reality technology, strapdown inertial navigating system and force-feedback technology.
本文介绍了一个结合增强现实、惯性导航和力反馈技术的体验平台。
An error estimate model of rotation vector was analyzed for the strapdown attitude algorithms. Based on this model, some kinds of high_accuracy strapdown attitude algorithms were deduced.
针对捷联惯导系统姿态算法分析了一种旋转矢量误差估计模型，并从该模型出发，推导了几种高精度的捷联姿态算法。
The introduction of the new algorithm is a new idea to calculate attitude error compensation of FOG strapdown inertial navigation(SINS) under the condition of high dynamic angular motion.
新算法的提出为高动态环境下光纤陀螺捷联系统的姿态误差补偿提供了一个新的思路。
The Edge Vector Test (EVT) is a very important and practical redundant management algorithm for Redundant Strapdown Inertial Measurement Sys-tems (RSIMS) composed of Two Degree of Freedom gyros.
对于由两自由度陀螺构成的冗余捷联惯性测量系统（RSIMS）来说，边缘向量检测（EVT）是一种非常重要和实用的冗余管理算法。
The Edge Vector Test (EVT) is a very important and practical redundant management algorithm for Redundant Strapdown Inertial Measurement Sys-tems (RSIMS) composed of Two Degree of Freedom gyros.
对于由两自由度陀螺构成的冗余捷联惯性测量系统（RSIMS）来说，边缘向量检测（EVT）是一种非常重要和实用的冗余管理算法。
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