inertial guidance

inertial guidance

美 　英

• un.〔空〕惯性制导
• 网络惯性导航；惯性导引；惯导

英汉解释

un.	1. 〔空〕惯性制导

英英解释

n.	1. navigation by conversion of the accelerations experienced into distances and directions.

例句

Rockets flew much faster and required inertial guidance for just a few minutes to put the weapon on a predictable ballistic path.

火箭的飞行相比以前要快得多，而且它仅需要几分钟的惯性制导就能把武器推送到一个可预测的弹道路径上。

Inertial guidance is often used in medium and long range missiles (over 40km say) when the intention is to hit a given map reference.

中远程导弹（比如说超过40公里）要想命中某一个给定的目标，经常采用惯性制导。

Transfer alignment is one of the key techniques in modern inertial guidance weapons.

传递对准是现代惯性制导武器的关键技术。

It also often includes global positioning systems (GPS) and inertial guidance systems (IGS) for tracking and positioning information.

它还常常包括全球定位系统和惯性指导系统，用来跟踪和定位。

Electromagnetic disturbance affect the performance of the inertial guidance test equipments and flight motion simulators.

电磁兼容性问题已经成为影响飞行器地面测试、仿真试验设备综合性能发挥的重要因素之一。

This paper introduced the self- stabilization method of feedforward control in the measurement ship with inertial guidance system.

介绍了具有惯性导航系统的大型舰艇上前馈控制的自稳定方法。

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

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。

It is claimed that the YJ-62 uses strap-down inertial guidance coupled with GPS, and active radar for the terminal phase.

据称YJ-62采用了惯性导航系统，并通过GPS系统进行修正，在飞行末段，使用主动雷达导引头。

The PL-12 does benefit from Russian technology, with the seeker and inertial guidance system provided by Moscow.

得益于俄罗斯技术，搜索器和惯性制导系统由莫斯科提供。

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

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。

This is the basic idea behind inertial guidance systems.

这是惯性制导系统，的基础概念。

Flight test analysis of an improved transfer alignment for missile strapdown inertial guidance system

弹载捷联惯性制导系统传递对准技术试飞验证

The Experiment and Simulation Research of Initial Alignment of the Strapdown Inertial Guidance System of Short Range Missile

近程导弹捷联惯导初始对准试验与仿真研究

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

初始对准误差对惯性制导误差影响的简化算法

NC processing technology for large single piece cast bracket of inertial guidance subassembly

大型铸件惯组支架的整体数控加工技术

EMC Analysis of the Controlling Device of Showing in Inertial Guidance System

惯性导航系统显示控制装置的电磁兼容性分析与设计

Evaluation model for error compensation of inertial guidance system

惯性制导系统误差补偿评估模型研究

Study on Redundant Technology in the Strapdown Inertial Guidance System

冗余技术在捷联惯导系统中的应用研究

The Development Tendency of Combination Technology of Strapdown Inertial Guidance and Navigation Satellite

捷联惯导与导航卫星组合技术的发展趋势

The Application of DSP in Strapdown Inertial Guidance System

DSP在捷联惯性制导技术中的应用

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

战术导弹惯性制导中的两种姿态角及其相互关系