惯性制导系统

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

捷联惯性制导系统的电路设计

On Circuit Design of 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 .

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

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

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

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 .

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 .

本文应用系统辨识和参数估计理论，提出了运载火箭的主动段距离惯性制导系统。

In this paper a distance-inertial guidance system in boost phase of the launch vehicle is presented by means of system identification and parameter estimation theory .

该系统具有光学系统运算速度快，对畸变目标识别能力高等优点，在导弹原有惯性制导系统上进行改进，成本低。

This system has the advantages of high operation speed and high discrimination . The cost will be low due to the betterment of missile inertial guidance system .

从3个方面对该问题进行了讨论：数字调平的原理与实现方法；捷联惯性制导系统双位置、零力矩法自对准的实现方法；

Three problems are discussed : the first is the theory and realization method of digital level , the second is the realization of auto-alignment with two-position-zero-torque method for strapdown inertial guidance system , and the third is the accurate position transition .

惯性制导系统初始对准的主要任务是精确确定载体坐标系和制导坐标系之间的初始方向余弦矩阵和载体的初始速度。

The main tasks of initial alignment of the SINS guidance system are to precisely determine the initial direction cosine matrix between the carrier body coordinate system and the guidance coordinate system , as well as the initial velocity of the carrier .

适合于机动弹道导弹的星光&惯性组合制导系统研究

Study on Stellar-Inertial Integrated Guidance System for Mobile Ballistic Missile

基于随动平台的天文-惯性复合制导系统在弹道导弹上的应用研究

On Celestial-Inertial Compound Guidance System Based on Follow-up Platform

星光-惯性复合制导系统

Hybrid Celestial-inertial Guidance System

仿真结果表明，天文-惯性复合制导系统可以有效地修正导弹的初始定位定向误差及初始对准误差。

Simulating results show that the celestial-inertial compound guidance system based on follow-up platform can measure the initial launch position errors and initial misalignments efficiently .

一种基于压电陀螺的捷联惯性测量与制导系统

A Strapdown Inertial Measurement and Control System Based on Piezoelectric Gyroscope

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

光学惯性制导和导航系统

Ce and navigation system integrated navstar hybrid inertial

本文介绍了一种由压电陀螺和石英挠性加速度计组成的捷联惯性测量与制导系统。

This paper presents a kind of inertial measurement system made of piezoelectric sensor and accelerometer .

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 .

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。

Quaternion method , which has been successfully applied to the Strapdown Inertial Navigation and Guidance for tens year , is classical .

在航天、航空以及航海领域，仿真转台作为研制和测试惯性导航及制导系统过程的重要设备，一直发挥着不可替代的作用。

Simulation table always plays the irreplaceable role as the key equipment in the design and test of the inertia navigation guide guidance and control system progress at the aerospace , aerial and nautical domain .

加速度计是最重要的惯性仪表之一，用于惯性导航和惯性制导系统。

The accelerometer is one of the most important inertial measurement units used in inertial navigation and guidance of a series of military systems .