1) intercepting warhead
拦截弹头
2) interceptor missile
拦截弹
1.
Attitude control for interceptor missile by combine control based on neural networks;
复合控制拦截弹的神经网络姿态控制
2.
Trajectory control for interceptor missile with combined control of lateral thrust and aerodynamics;
直接力与气动力复合控制拦截弹轨迹控制
3.
Based on infinite interpolation theory and multi-block grid technique,construction grid of interceptor missile with multiple attitude control motors was generated.
基于无限插值理论和多块网格技术,生成了带多姿控发动机的拦截弹结构体网格。
3) Interceptor
[英][,ɪntə'septə(r)] [美]['ɪntɚ'sɛptɚ]
拦截弹
1.
Modeling of Stability Control System for Blended Control Interceptor;
复合控制拦截弹的稳定控制系统数学模型的建立
2.
Research on Guidance Accuracy of Endo-Atmospheric Blended-Control Interceptor;
燃气动力／空气动力复合控制拦截弹的制导精度研究
3.
Aiming at enemy interceptor from different direction,a kind of maneuver penetration strategy used for terminal stage of missile with lateral thrust was put forward.
针对敌方不同来袭方位的拦截弹,提出了一种可用于导弹末段侧向力机动的突防方案。
4) antimissile interceptor
拦截弹
1.
Optimization of inverse design of antimissile interceptor based on physical programming;
基于物理规划的拦截弹反设计优化方法
2.
To meet the requirements of the attack and defense simulation of the ballistic missile,the mimetic designment methods of the antimissile interceptor is discussed based on the datum and simulation analysis.
根据弹道导弹攻防仿真需求,在资料分析和性能仿真基础上对拦截弹技术状态和性能进行了分析研究,提出了拦截弹反设计方法,拦截弹性能分析和反设计模型综合考虑了拦截弹总体、气动、制导控制、固体火箭发动机等方面。
5) intercept missile
拦截导弹
1.
The blended control system of an intercept missile by means of combining the aerodynamics control with reac- tion jets control is studied in this paper.
以拦截导弹直接力和气动力的复合控制系统为研究对象,首先建立了导弹的数学模型。
2.
The compound control system of an intercept missile by means of combining the traditional aerodynamics control with reaction jets control is studied in this paper.
以大气层内拦截导弹侧向直接力和气动力的复合控制系统为研究对象 ,首先分析了侧向喷流与来流的干扰现象 ,建立了通过干扰放大因子来描述的侧喷与来流的干扰模型和侧向直接力与气动力的复合控制模型 ,将复合控制系统分解为直接力子系统和气动力子系统 ,并分别针对侧向直接力和气动力的特点设计了直接力控制子系统和气动力控制子系统 ,仿真分析了两个子系统的性能及复合系统的性
3.
This paper mainly works on the problems of modeling, control and guidance for an intercept missile based on side jet and aerodynamics compound control.
本文的研究主要是围绕着直接力/气动力复合控制拦截导弹的建模、控制和制导所展开的。
6) Missile interception
导弹拦截
1.
As one of the indispensable technologies in the future war, missile interception has become a researching focus in the military field.
导弹拦截作为未来高技术战争的一项必备技术,已成为世界军事领域研究的焦点。
补充资料：弹头烧蚀(见弹头防热)
弹头烧蚀(见弹头防热)
warhead ablation
dantou shaoshi弹头烧蚀(warhead的lation)见弹头防热。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条