惯性制导

DSP在捷联惯性制导技术中的应用

The Application of DSP in Strapdown Inertial Guidance System

这是惯性制导系统，的基础概念。

This is the basic idea behind inertial guidance systems .

和平保卫者导弹惯性制导器件和系统设计的进展

Evolution of The Peacekeeper Inertial Guidance Components and System Designs

末制导炮弹惯性制导仿真及横向散布研究

Terminal-guided Projectile Inertial Navigation Simulation and Lateral Distribution Study

机载导弹惯性制导装置生产测试工艺研究

Technological Study on Production Test of Airbone Missile IGS

惯性制导系统误差补偿评估模型研究

Evaluation model for error compensation of inertial guidance system

战术导弹惯性制导中的两种姿态角及其相互关系

Relationship between Two Kinds of Attitude Angle in the Inertial Guidance of Tactical Missile

空空导弹惯性制导系统设计的几个问题

Some Problems of IGS Design in Air-to-air Missiles

光学惯性制导和导航系统

Ce and navigation system integrated navstar hybrid inertial

惯性制导平台台体有限元分析

Finite Element Analysis of the Inertial Navigation Platform

捷联惯性制导系统的电路设计

On Circuit Design of Strapdown Inertial Guidance System

陀螺惯性制导及其军事应用

Inertia guidance of gyroscope and its military application

初始对准误差对惯性制导误差影响的简化算法

A Simplified Algorithm for Calculating the Influence of Initial Alignment Error on Inertial Guidance Error

惯性制导中的精确引力模型

The precise gravity modeling for inertial guidance

利用飞行试验数据对惯性制导系统误差进行分析鉴定的方法

The Methods of Analysis and Evaluation for Errors of Inertial Guidance System in Flight Test

对无陀螺捷联惯性制导系统中的数值积分方法的讨论

Discussion of the Numerical Integration Algorithm Used in the Gyroscope Free Strapdown Inertial Navigation Guidance System

反辐射导弹惯性制导段拉制参数的优化

The Optimization about the Control Parameters of the Anti-radiation Missile During the Period of Inertial Guidance

捷联式惯性制导的发展

The Evolution of Strapdown Inertial Guidance

星光-惯性制导地面仿真试验计算机系统软件设计

Software design of the computer system for simulation tests of the starlight - inertial guidance system

运载火箭的距离惯性制导

Distance-inertial guidance of the launch vehicle

本文讨论远程弹道导弹惯性制导系统的误差传播特性。

This Paper describes the error propagation properties of IGS ( Inertial Guidance System ) for ICBM .

本文研完惯性制导系统工具误差的自适应估计问题。

This paper studies the problems of adaptive estimation of the instrumental error to the guidance system .

无线电惯性制导系统

Radio inertial guidance system

作为惯性制导与导航系统中的主要器件，加速度计和陀螺仪一直是世界上各发达国家研究的热点。

As the key sensor of inertial navigation system , accelerometer has been under intense research in developed countries .

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。

The paper introduces a very low cost strapdown inertial guidance system consisting of piezoelectric gyros and low cost accelerometers .

舰载弹用捷联系统初始对准时陀螺误差的估计抗雷达关机的无陀螺捷联惯性制导方案探讨

Discussion on the Guidance scheme of Gyroscope Free Strapdown Inertial Navigation System ( GFSINS ) used in Anti-turn off of Radar

基于惯性制导工具误差模型，推导出存在工具误差时的再入点运动参数模型。

Based on the inertial guidance instrument error model , the model of reentry point 's parameters is established in this paper .

系统的精度比现有惯性制导系统的精度有较大的提高。

The accuracy of the distance-inertial guidance system in boost phase is much higher than that of the current inertial guidance systems .

介绍了一种弹载捷联式惯性制导系统传递对准改进设计方案，描述了在运输机上进行试飞验证的方法和结果。

The paper described an improved transfer alignment scheme for missile Inertial Guidance System , and presented the flight test procedure in a transporter .

在惯性制导系统中，有一个旋转的轮，至少当制导系统里存在，机械的轮子。

In inertial guidance systems , you have a spinning wheel , at least in the days that the guidance systems had mechanical wheels .