inertial navigation system

Design and Realization of Gravity Aided Inertial Navigation Simulation Demo System

重力辅助导航仿真演示系统设计与实现

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Sculling Compensation Algorithm s in Strapdown Inertial Navigation System

基于对偶性原理捷联惯导划船误差补偿优化算法

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Tilt Angle Error Model of Inertial Navigation System

惯性导航系统水平角误差计算机辅助分析与建模

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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.

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Approach Certain Problems of Overall Design of Inertial Navigation System Three-Axis Test Table

惯性系统三轴综合测试转台总体设计若干问题的探讨

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A method for processing the problem resulting from master inertial navigation system ( MINS) data delay in transfer alignment was presented.

计算机仿真结果表明对数据滞后进行补偿后改善了传递对准的性能。

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Design for a data acquisition module of the accelerometer in the inertial navigation system

惯导系统中加速度计采样模块的设计

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A real-time software digital simulation method for strapdown inertial navigation system ( SINS) of a ground-to-ground missile is introduced.

介绍一种在PC机上对地对地导弹捷联惯导系统实时软件进行数字仿真的方法。

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a new method of 3 rd order minimal parameter solution for the orthogonal matrix differential equation is modified and used to solve the quaternion differential equation, and the numerical simulation is done in the strap-down inertial navigation system ( sins).

对一种求解正交矩阵微分方程的三阶最小参数方法进行改造，将其用于四元数微分方程求解，并对其在捷联惯性导航系统姿态矩阵实时求解中的应用进行了仿真。

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on basis of that, adopting the above-mentioned research results, the soft system of the strapdown inertial navigation system is designed and implemented.

在此基础上，应用上述研究成果，设计并实现了捷联惯性导航软件系统的原型。

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The Design of Inertial Navigation System Simulator Based on Submarine Space Motion

基于潜艇空间运动的惯性导航系统模拟器设计

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On the Theory of Optical Gyro Rotating Inertial Navigation System

光学陀螺旋转惯导系统原理探讨

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The similarities between coning compensation algorithm and sculling error compensation algorithm in strapdown inertial navigation system are introduced.

介绍了捷联惯导系统中圆锥补偿算法与划船误差补偿算法之间的相似性；

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Integrated Optical Gyro ( IOG) based on Sagnac effect is a type of inertial angular rate sensor and plays an important role in modern inertial navigation system.

集成光学陀螺（IOG）是一种基于Sagnac效应的惯性角速度传感器，在现代惯性导航系统中具有重要作用。

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The scale-factor error of inertia component of Inertial Navigation System ( INS ).

阐述基于模糊优化算法的导航系统 惯性元件 误差 补偿方法.

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The platform inertial navigation system used peg-top to stabilize the loop through platform and control the angular speed of the platform track navigation coordinate system.

平台式惯导系统将陀螺通过平台稳定回路控制平台跟踪导航坐标系在惯性空间的角速度。

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The Evaluation of Position Accuracy and Its Radius of the Circle of Equal Probability of Ship Inertial Navigation System

舰船惯性导航系统定位精度评定及其圆概率半径

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In the thesis, the technology of initial alignment and transfer alignment of the inertial navigation system of the carrier borne plane when the aircraft carrier is moored or is cruising is researched.

本文以舰载机为研究对象，系统全面地研究了其惯导系统在航母系泊和巡航条件下的初始自对准技术和传递对准技术。

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Application of LTN-72 Inertial Navigation System to the Flight Experiment for the Calibration of a Satellite-borne Remote Sensor

LTN&72惯导设备在空间遥感器航空校飞中的应用

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Inertial navigation system with the character of good covert and autonomous, can meet the navigation requirements of underwater vehicle to long periods sneak in blue water.

水下运载体的主要定位方式为惯性导航，其提供的导航信息具有隐蔽性好，自主性高的特点，能够满足需长期潜行的水下载体对导航的要求。

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Methods of error compensation for azimuth holding system in an INS ( inertial navigation system ) are presented.

给出了陆用 惯性导航 系统方位保持仪的误差 补偿方法 .

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Method of Sea Experiment for Inertial Navigation System on All-aluminium High Speed Boat Research

全铝制高速艇惯性导航系统海上试验方法研究

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Design and Development on Calibration and Testing Software of FOG Strapdown Inertial Navigation System

光纤陀螺捷联系统标定测试软件的设计与开发

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Four Two-Dimension of Freedom Gyros Inertial Navigation System Redundant Design Analysis

四个双自由度陀螺捷联惯导系统冗余设计研究

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Technique Research for Torpedo Inertial Navigation System Based on Laser Gyros

基于激光陀螺的鱼雷惯导系统技术研究

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To improve the navigation accuracy of strapdown inertial navigation system ( SINS) in long time flying, the three general errors of attitude, velocity and station and system error were analyzed in this paper.

为提高捷联惯导系统（SINS）长时间工作的导航精度，分析了SINS的姿态角、飞行速度和定位三类基本误差，以及系统误差的表示方法。

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The stability of ground-to-ground missile's inertial surveying system has a direct impact on the accuracy of the inertial navigation system of missiles.

地地导弹惯性测量系统的稳定性直接影响导弹惯性导航系统导航的准确程度。

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Then it designed and programmed an algorithm of Strap-down Inertial Navigation System with all kinds of parameter interface which is suitable for this paper in order to make a research on the simulation of navigation calculation under different simulation modes.

然后设计编写一种适合于本课题的具有各种参数接口的捷联惯导导航算法，研究不同仿真模式下的导航解算仿真。

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The paper introduces the designing techniques of general hign-performance multiplex pulse acquisition in strapdown inertial navigation system ( SINS), and mentions the designing methods with PLD ( Programmable Logic Device) to perform the main function.

阐述了应用于捷联式惯性导航系统（SINS）中的通用高性能多路脉冲信号采集器的具体工程设计，提出了完成其主体功能的可编程逻辑器件（PLD）详细设计方法。

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Integration of global positioning system with inertial navigation system

全球定位系统与惯性导航系统的组合系统

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