战术导弹

某战术导弹飞控系统BIT分析

The BIT Analysis of Control System of a Tactical Missile

基于UML的战术导弹遥测数据处理系统设计方法研究

Research on Design Method of Tactical Missile Telemetry Data Processing System Based on UML

战术导弹CFD软件求解器开发与应用

Development and Application of CFD Solver for Tactical Missile

界面化、自动化的战术导弹CFD系统平台

Graphic and Automatic Tactical Missile CFD Systemic Platform

基于GA的战术导弹对疏散型集群目标靶场效能优化

Optimization of tactical missile effectiveness in absence of air defenses to group targets based on genetic algorithm

阐述了协方差分析描述函数法（CADET）的主要内容，并结合一战术导弹非线性模型，展示了CADET法在导弹命中概率评估中的应用。

The main contents of Covariance Analysis Description Function Technique are interpreted .

本文结合互联网技术与故障诊断技术，实现基于Web的战术导弹武器系统的远程故障诊断，使得故障诊断效率及资源利用率得到有效提高。

The thesis apply the skills of internet and fault diagnosis to achieve long range fault diagnosis of the Web-based tactical missile weapon system , it will advance the efficiency of fault diagnosis and the availability of resources .

通过对几种典型的陀螺稳定方案的比较，选定目前在大多数战术导弹上获得广泛应用的速率陀螺稳定平台方案，并选用高速数字信号处理器（DSP）构成稳定回路的数字控制系统；

In the paper , a few typical gyro stabilization platform projects are compared firstly , and choose rate gyro stabilization platform project , the project has been in wide use in tactical missile , simultaneity digital controller of stabilization loop adopt high speed digital signal processor .

结果表明，石墨渗铜材料具有较好的抗热震性能，解决了高性能战术导弹和航天飞行器高压强大流量固体火箭发动机（SRM）喉衬材料的关键技术。

Results indicate that copper impregnated graphite has good thermal shock resistance , which solves the critical technique of throat liner material used in high performance tactical missile and space vehicles with high pressure , high flow rate SRM .

设计了VSCMGs的操纵律.战术导弹制导律设计

Design of Guide Law for Tactical Missile

基于知识的战术导弹二级维护设备IDTS-1介绍

Knowledge-based tactical missile two-level maintenance equipment idts-1

论述了故障模式影响及危害性分析（FMECA）的目的和意义，尤其强调了战术导弹全弹FMECA对提高导弹可靠性的作用。

The purpose and mean of failure mode effect and criticality analysis ( FMECA ) were presented in this paper , and the function of FMECA for whole tactical missile to improve the missile reliability was stressed .

1953年，第一种使用可贮存推进剂（硝酸和碳氢燃料）的战术导弹R-11被研制出来，射程270千米。

In1953 the first tactical missile using a storable propellant ( nitric acid and carbon-hydrogen fuel ), the R-11 , was created with a range of270 km .

战术导弹反辐射战斗部分析研究

Analysis and Research on Anti - radiation Warhead of Tactical Missile

战术导弹武器装备退役的模糊聚类分析

Analysis of Retirement of Tactical Missile Weaponry Based on Fuzzy Cluster

战术导弹对目标打击的最优分配策略研究

Study on the Optimal Allocation Policy of Tactical Missiles to Targets

地地战术导弹飞行可靠性指标评定方法

Estimation Method for Flight Reliability of Surface to Surface Tactical Missile

喷流姿控战术导弹三维气动力数学模型

Three Dimensional Aerodynamic Mathematical Model for Tactical Missiles with Jet Steering

战术导弹自动测试系统体系结构的选择

Selection of the Architecture of a Tactical Missile Automatic Testing System

战术导弹武器系统抗干扰性能综合评定

Synthetic evaluation of ECCM performance of the tactical missile weapon systems

地地战术导弹武器系统信息作战效能评估

Operational Effectiveness Evaluation on Information Operation of Surface-to-surface Missile Weapon System

某小型战术导弹系统误差分析方法研究

A study on methods of error analysis of tactical missile system

中远程战术导弹预测命中点的计算

Calculation on Predictive Impact Point of Intermediate and Long Range TBM

战术导弹贝叶斯检验方案设计与应用研究

Plan Design and Application Research of Bayes Inspection for Tactical Missile

战术导弹指挥员指挥能力模糊评估模型

Fuzzy Evaluation Model of Command Ability for Commander of Tactical Missile

战术导弹垂直发射控制的输出解耦变结构方法研究

Variable-Structure Control of Vertical Launching Missile Based on Output Decoupling Method

具有全动翼的战术导弹的反操纵气动问题

Aerodynamical Problem of the " Anti-Control " of Tactical Missiles with Moving-Wings

高能激光武器反战术导弹的技术分析

Technical analyses using high laser weapon against tactical ballistic missile

战术导弹训练仿真器的设计与实现

The Design and Realization of Training Simulator for Tactical Missile

战术导弹动力装置靶场试验与评定

Range test and evaluation for propulsion system of tactical missile