missile

Dynamical Property Analysis of Un-Rounded Cross Section Airframe for Aerodynamic Missile;

非圆截面飞航导弹弹体动力学特性分析

Study on CAD software for analyzingaerodynamic missile s control loops;

飞航导弹控制回路分析CAD软件研究

Development of thermal protection techniques for aerodynamic missile

飞航导弹热防护技术发展趋势

Vertical Guidance Design of Cruise Missile Based on Inertial Vertical Velocity;

利用惯性垂速进行飞航导弹纵向导引设计

Application database in simulation modeling for cruise missile;

数据库在飞航导弹仿真建模中的应用

To meet the cruise missile s air-to-surface attack requirement,specified impact angle guidance law is presented based on line of sight (LOS) information framework.

根据飞航导弹对面攻击的需要,针对可以获取的信息,设计了视线角信息框架下的双平面导引规律,以实现指定入射角的攻击,并从理论上进行了分析。

Correcting SINS gyro drift in winged missile by star sensor;

在飞航导弹中用星敏感器修正捷联惯导陀螺漂移

Laser weapon and defense techniques of winged missile;

激光武器及飞航导弹的防护技术

Simulation software of integrated guidance for long-range winged missile;

远程飞航导弹组合制导仿真软件

The Design of Guidance Law of Aerodynamic Missile Based on Intelligent Sliding-mode Variable Structure

飞航导弹智能自适应滑模制导律设计

Simulation of INS/GPS Integrated Navigation in Aerodynamic Missile

飞航导弹INS/GPS组合制导仿真分析

Autonomous Navigation Modification Based on Passive Observation to Feature Target for Cruise Missile

飞航导弹地标被动观测自主导航修正技术

Application of Unscented Kalman Filter in Geomagnetic Navigation for Aerodynamic Missile

Unscented卡尔曼滤波在飞航导弹地磁导航中的应用

Application database in simulation modeling for cruise missile

数据库在飞航导弹仿真建模中的应用

Research on Object - Oriented Simulation Modeling Method for Cruise Missile

飞航导弹面向对象仿真建模方法研究

Research on Safety Control Factors of Winging Missile Developing Enterprises

飞航导弹研制企业安全控制要素研究

ECM system of aircraft type missile and its development trend

飞航导弹电子对抗体系及其发展趋势

Study of Blockage Probability of Aerodynamic Missile with Cluster Warhead to Block Runway

飞航导弹子母弹对机场跑道封锁概率研究

RESEARCH OF GUIDANCE AND CONTROL FOR BTT WINGED MISSILE

倾斜转弯飞航导弹的制导与控制问题研究

Real-Time Simulation for a Certain Aerodynamic Missile by YH-F2

利用银河仿真机Ⅱ对某飞航导弹进行实时仿真

An Investigation into Soft-killing Effectiveness Evaluation for Aerodynamic Missile Based on Operation Simulation

基于仿真的飞航导弹软杀伤效能评估探讨

A STUDY FOR EVALUATION METHOD OF THE HIT PROBABILITY BY SINGLE SHOT FOR CRUISE MISSIE

评定飞航导弹单发命中概率的方法研究

Design on Altitude Control System of Cruise Missile Based on Fuzzy Logic;

基于模糊逻辑的飞航导弹高度控制系统设计

Evaluation Method of General Schemes of Missile: Theory and System Implementation;

飞航导弹总体方案评价方法研究及系统实现

Research on Supporting Technologies to Conceptual Design of Missile;

飞航导弹方案设计的关键支撑技术研究

An Adaptive Attitude Control Law for Air-launched Cruise Missile

空射飞航导弹姿态控制的一种自适应方法

an aerodynamic missile

飞航式导弹, 有翼导弹