Backstepping Adaptive Control of Internal Mass Motion of Ballistic Missile
弹道导弹变质心反推自适应控制
A design of nonlinear control system for long distance aerodynamic missile
远程飞航导弹的非线性控制系统设计
The main issues of penetration for aerodynamic missile have been reviewed.
概述了飞航导弹突防的主要问题。
Fuzzy Evaluation Model of Command Ability for Commander of Tactical Missile
战术导弹指挥员指挥能力模糊评估模型
The Analysis on Dispersion Characteristic of Aerial Defence Missile Warhead
防空导弹战斗部破片飞散特性分析
The situation of cruise missile's actual effect in the Gulf War is outlined.
简述了海湾战争中飞航导弹的实战情况。
Introduction to Penetration Technologies and Tactics for Aerodynamic Missile
飞航导弹突防技术与战术导论
RESEARCHING AND ACCOMPLISHING FOR HOMING MISSILE ATTACKING MANEUVERING TARGET
自寻的导弹攻击机动目标的最优制导规律的研究及实现
Passive Acoustic Detection and Classification Techniques on the Cruise Missile
巡航导弹的被动声检测与分类技术
Technical approach to improve the maximum powered range of IR air to air missile
提高红外空对空导弹动力射程的技术途径
Research on Penetration Adaptive Control Technology for Lap Weld of Missile Shell
导弹壳体搭接焊缝的熔深适应控制技术研究
New Scud missiles, missile like hair on the hair, the missile power free control.
新增飞毛腿导弹，导弹想发就发，导弹威力自由控制。
Missile flight control was performed using aerodynamic vanes and gas control jets.
导弹的飞行控制是由气动翼和姿态控制燃气喷口实现的。
Analysis on estimates related problems in acquisition cost of missile weapon system
导弹武器系统采办费用估算有关问题分析
RESEARCH OF ACTUATOR IN FULLDISTANCE CONTROL OF TACTICAL SURFACE TO SURFACE MISSILE
战术地地导弹全程控制执行机构研究
Application of Angular Accelerometer in Tactical Missile Guidance and Control System
角加速度计在战术导弹制导控制系统中的应用
The interception of a missile by another missile or an aircraft by another aircraft.
截击，拦截一导弹为另一导弹或一飞机为另一飞机所拦截
Damaging Evaluation of Air to Surface Missile Against Mobile Missile Armament System
空地导弹对机动导弹武器系统毁伤能力评估
Yes. And from this state of accelerated motion, it launches a nuclear missile.Sokolov
然后在这种加速运动的状态中发射核弹。
Radar active decoy system and simulation about antiradiation missile counttechnology.
雷达有源诱偏与反辐射导弹对抗仿真技术
This missile has been equipped with the most advanced lasers to control and guide it.
这种导弹安装了最先进的激光制导设备。
Adaptive Flight Control System of Air to Air Missile with Quantitative Feedback Theory
空空导弹自适应飞控系统的定量反馈理论设计
A solid rocket booster causes the initial acceleration and launch of the cruise missile.
一个固体火箭推进器给导弹以初加速度并将其发射出去。
Analyses on the missile's aerodynamic coupling control system with large angle of attack
大迎角下导弹气动耦合控制系统分析
A rapid iteration algorithm adapting to ballistic missile trajectory design is presented.
摘要提供了弹道导弹弹道设计的一种快速迭代方法和模型。
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