导弹制导系统

应用SLAM法对导弹制导系统的统计分析

A statistical analysis of missile guidance system by the slam method

战略导弹制导系统精度评估方法及应用研究

Strategy Missile Guidance System Accuracy Evaluation Method and Application Research

防空导弹制导系统一体化仿真系统框架

The Framework of Integrated Simulation System for Guidance System of Anti-aircraft Missiles

天线罩影响下导弹制导系统的分析与鲁棒设计

Analysis and Design of Missile Guidance System with Radome Effects

数字化设计平台在导弹制导系统研制中的应用

Application of Digital Design Platform to Missile Guidance System Design

红外导弹制导系统的半实物仿真系统设计

Design of Semi Physical Simulation System for Missile Infrared Control and Guide System

导弹制导系统快速原型研究

Research on Rapid Control Prototyping of Missle

防空导弹制导系统综合效能评估指标体系研究

Research on Comprehensive Effectiveness Evaluation Criteria System of Guidance and Control System of Anti-aircraft Missile

研制出了进行战术导弹制导系统研究的六自由度仿真软件包，共由十多个模块组成。

There are eleven pieces of models about the missile guidance loop in the simulation software .

质量物元分析法在某型导弹制导系统质量评定中的应用

Application of matter elements analysis method to quality evaluation of guidance system in a certain missile

提出了超高速导弹制导系统方案。

The project about the system of control and guide for super-speed guided missile is brought forward .

对雷达和导弹制导系统的设计师来说，隐身飞机的目标特征信号是诱人的。

The radar target signatures of the stealth aircraft are attractive to designers of radar and missile guidance .

导弹制导系统的功能是引导导弹以最大的命中概率击中目标。

Missile guidance system function is to guide the missile to hit the target with the highest probability .

随着导弹制导系统的日趋复杂，试验的费用也在不断增加。

As the missile guidance system becomes more and more complicated , the cost of the test is also continually increasing .

提出了对新一代空空导弹制导系统的主要战术技术要求、实现这些新战术要求的技术途径和战术空空导弹制导系统设计中几个矛盾的处理。

According to tactical requirements of the air-to-air missile guidance system , a compromise way to meet these needs is proposed .

为了使导弹制导系统具备良好的鲁棒性，本文提出用滑模变结构控制理论设计末端导引规律。

Sliding-mode variable structure control is applied to design a guidance law so that the guidance law is robust to certain disturbances .

本文论述了战略导弹制导系统精度评估方法，并分析了影响制导精度的各种因素；

In this paper , we discuss the accuracy evaluation methods of guidance system and analyse a varieties of factors of affecting guidance accuracy .

提出了一种用于空空导弹制导系统动态仿真测试的数字成像导引回路设计与实现方法。

A design and implementation method is put forward which is applied to digital imaging guidance loop used in dynamic simulation for air-to-air missile guidance system .

本论文选题来自于探测制导与控制技术实验室建设中的导弹制导系统实验项目，主要研究了此实验项目中的视景仿真部分。

This dissertation is supported by missile guidance system experimental project of lab building , the visual simulation of this project is studied in this dissertation .

利用物元分析理论建立某型导弹制导系统的质量数学模型，给出了评定准则。

This paper uses theory of matter elements analysis to establish the mathematical models for the quality of guidance system in a certain missile , and presents an evaluation regulation .

从地地导弹制导系统的发展历程，论述了地地导弹制导技术的未来趋势，讨论了激光精确制导技术在地地导弹末制导中的应用可行性。

In this paper , from the development of the surface to surface missile guidance , the future direction of the surface to surface ( missile ) guidance is discussed .

该模拟器应用于导弹制导系统半实物仿真实验，采用测频引导方式产生目标源信号，利用天线阵列模拟目标的角位置。

Applied to hardware-in-the-loop simulation for guidance and control systems , the simulator generates source signals by means of IFM and simulates the angular position of the targets by an aerial array .

在全系数自适应控制方法基础上，利用低阶等效和规范化模型方法，对自寻的导弹制导系统设计了一种新的自校正控制器。

For the homing missile control system , based on the all - coefficient adaptive control method , presents a new self-tuning controller based on lower order equivalence and the normalized model method .

三叉戟Ⅱ导弹的制导系统MK-6

The Trident ⅱ Guidance System MK-6

针对参数方块网格法每个数组只能生成两个主要特征的缺点，本论文提出了一种改进算法&三角参数方块网格法，并利用此方法生成了导弹制导仿真系统的10Km×10Km地形数据。

In order to overcome the disadvantage that each array of parameter quadrate mesh only create two main character , an improved algorithm is put forward in this dissertation .

结合BTT控制的特点，推导了极坐标系下的弹目相对运动方程，建立了BTT导弹制导控制系统的数学模型，在此基础上对BTT比例导引律进行了分析。

Considering the characteristic of BTT control , the relative motion equation is established in the polar coordinate , based on which the mathematical model of BTT guidance system is obtained . Then BTT PNL is deeply analyzed .

远程多功能导弹寻的制导系统技术研究

A technical study of seeking guidance system of remote multifunction missile

新型防空导弹制导控制系统展望

The prospect for guidance control system of a new air-defence missile

空射倾斜转弯导弹制导控制系统设计

Design of Guidance and Control of Air - Launched BTT Missile

导弹制导控制系统中自适应技术仿真研究

The Simulation Study of Adaptation Technology in Missile Guidance Control System