制导与控制系统

惯性导航系统（INS）以其自主的工作能力广泛应用于军事武备的导航、制导与控制系统和国民经济的诸多领域。

Inertial navigation system ( INS ) is used widely in many military and civil scopes because of its ability of independent operation .

高速再入飞行器的制导与控制系统设计

Design of guidance and control system for high speed reentry aerocraft

设计注重了导航计算机系统的可扩展性，可应用于多种微小型GPS/SINS，DGPS/SINS/MC等组合导航、制导与控制系统。

The computer can be used in GPS / SINS , DGPS / SINS / MC due to its expansibility .

弹载计算机是现代导弹制导与控制系统的核心装置，其性能的好坏，直接关系到精确制导的精度和杀伤目标的概率。

The missile-borne computer is key installment of the modern missile guidance and the control system , its performance quality relates the precision of guidance and the probability of target damage directly .

动态目标跟踪一直是航空、航天、武器制导与控制系统的重要组成部分，它的精确定位实时跟踪，可有效地提高系统的智能控制效率。

Dynamic target tracking has been the important composing of the aviation , spaceflight , weapons guidance and control system , its precise location tracking effect can effectively improve the intelligent controlling efficiency of the system .

在航天航空领域中，导航、制导与控制系统的精密程度往往决定着整个导弹、航天器或航空器的性能，其对产品性能和质量的要求更是精确细密、慎之又慎。

In the field of astronautic and aviation , the precision degree of navigation , guidance and control system often determines the whole capability of a missile , spacecraft or aircraft , the demand of its capability and quality is extremely accurate and precise .

制导与导航控制系统

Guidance and navigation control system

本文主要以某型反辐射导弹为背景研究其制导律与控制系统。

In this paper , the design of guidance law and control system for the anti-radiation missile is researched .

本文针对深空探测器导航、制导与控制分系统进行了方案设计与仿真研究。

In view of the navigation , guidance and control subsystem of deep space probe , the program design and the simulation research are carried out .

对动能拦截器末段拦截的制导与姿态控制系统进行建模和仿真分析。

This paper investigated the modeling and simulation of the guidance and the attitude control systems of kinetic kill vehicle in the terminal process of interception .

仿真结果也验证了动力下降段的制导、导航与控制系统的设计的合理性。最后，进行了终端着陆段的制导、导航与控制系统设计。

The design is also verified by numerical simulations . Finally , the GNC system for the terminal descent phase is proposed .

构建了微小型飞行器（MAV）导航、制导与控制（GNC）系统。

The guidance , navigation and control ( GNC ) system of micro air vehicle ( MAV ) is constructed .

本文介绍中国计划中的第一个绕月探测器的GNC（制导、导航与控制）系统，简述其任务和性能指标，系统组成，工作模式，以及系统设计中解决的主要问题。

This paper presumes the GNC system of the first lunar explorer in China , in the works , putting forward to its system mission , performance index , system composition and operation modes . It also introduces the key technology in the system design .

还述及了该公司是如何解决铜斑蛇制导炮弹的精确制导与控制系统安全承受炮射时高达9000g的加速度过载这一技术难题的。

It also deals with Martin 's successful solution to the technical challenge of making Copperhead 's precision guidance and control systems to survive the high acceleration of up to 9000 g imposed by the firing from cannons .