1) winged missile target
飞航导弹目标
1.
The RCS of winged missile targets with three typi ca l shape warheads are calculated with all kinds of high frequency methods in the high frequency region,and the calculated results are proved efficiently by measu red results.
对处于高频区的导弹目标的电磁散射特性进行了研究分析,综合运用各种高频方法,计算了三种典型形状弹头的飞航导弹目标的雷达散射截面,并经过了文献中给出的测量结果的验证。
2) aerodynamic missile
飞航导弹
1.
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
2.
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
3.
Development of thermal protection techniques for aerodynamic missile
飞航导弹热防护技术发展趋势
3) Cruise Missile
飞航导弹
1.
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
2.
Application database in simulation modeling for cruise missile;
数据库在飞航导弹仿真建模中的应用
3.
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。
4) winged missile
飞航导弹
1.
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
2.
Laser weapon and defense techniques of winged missile;
激光武器及飞航导弹的防护技术
3.
Simulation software of integrated guidance for long-range winged missile;
远程飞航导弹组合制导仿真软件
6) cruise missile
飞航式导弹
1.
Comparing with normal ballistic missile, the lateral dynamical property analysis for cruise missile is more complex.
相对于常见的圆截面弹体的动力学特性分析而言,非圆截面弹体的动力学特性分析有其特殊之处;而对于飞航式导弹其侧向的动力学特性分析方法与一般的弹道式导弹相比较为复杂。
补充资料：无航
1.没有船。
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参考词条