1.
Application of Gain Scheduling on Flight Control System of Missile
预定增益理论在导弹飞行控制系统中的应用
2.
Design of Missile's Flight Control System Based on PSO Algorithm
基于粒子群算法的导弹飞行控制系统设计
3.
Design of flight training bomb's connected control cabin of guided bomb
制导炸弹飞行训练弹交联控制舱设计
4.
Research of Dynamic and Control of Spinning Ballistic Missile;
弹道导弹滚动飞行动力学与控制研究
5.
Research of Simply Guided Bomb Flight Control System Simulation;
简易制导炸弹飞行控制系统仿真研究
6.
Study on Control System Failure Mode during Air Defense Missile Flight Test
防空导弹飞行试验控制系统故障模式研究
7.
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
8.
Research on the Whole Flying Trajectory Simulation System of Command Guided Antiaircraft Missile
指令制导防空导弹全弹道飞行仿真系统研究
9.
guided in first part of flight but falls freely as it approaches target.
飞行的第一阶段受控制，但在接近目标时自由降落的导弹。
10.
a rocket-propelled missile whose path can be controlled during flight either by radio signals or by internal homing devices.
一种由火箭发射器推动的导弹，这种导弹的飞行路径可以由无线电波或者国内设计者控制。
11.
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
12.
Application of Fuzzy Control in Automatic Control System of Aerodynamics Missile
模糊控制在飞航导弹自动控制系统中的应用
13.
MIRV (multiple independently targeted reentry vehicle)
多弹头分导再入飞行器（多弹头导弹）
14.
The simulation result shows that the proposed overload control of the anti-ship missile can realize a flight by higher and lower trajectory successfully.
仿真结果表明,论文提出的反舰导弹过载控制,可以成功地实现高低弹道的飞行。
15.
flying bomb (missiles resembling aircraft)
飞弹（飞机的导弹）
16.
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
17.
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
18.
Analysis for Control Method in Autopilot System of Aerodynamics Missile
飞航导弹自动驾驶仪系统控制方案研究