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1)  suspension interception missile
悬浮式拦截弹
1.
Based on this,center position of the suspension interception missile is ascertained.
悬浮式拦截弹是水面舰艇拦截鱼雷的常用武器,首先从直航雷的相遇三角形命中目标条件出发,推导出鱼雷相对舰艇的正常提前角,从而确定鱼雷在被发现点的最大航向角范围。
2)  suspended depth charge
悬浮式深弹
1.
When the suspended depth charge is used to explore the torpedo, how to estimate the range of course angle correctly becomes the key point to lay the suspended depth charge accurately, if the distance to the aim can only be estimated by the experience of sonar soldiers.
在悬浮式深弹反鱼雷时,若只能根据声纳兵的经验估计鱼雷距离,如何正确估计鱼雷航向角范围就成为正确布放悬浮式深弹的关键。
2.
Evasive maneuver is one of key problems a surface ship faces while releasing suspended depth charge to intercept a torpedo.
水面舰艇使用悬浮式深弹拦截鱼雷时如何进行规避机动是舰艇防御鱼雷的重要问题之一。
3.
Based on the structure and working principle of anti-torpedo system of suspended depth charge,operational effectiveness model of anti-torpedo system of suspended depth charge is proposed.
基于悬浮式深弹反鱼雷系统的组成和工作原理,提出了悬浮式深弹反鱼雷系统的作战效能评估方法。
3)  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。
4)  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。
5)  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。
6)  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。
补充资料:悬浮
分子式:
CAS号:

性质:固体微粒分散在流体中称为悬浮。例如,以固体微粒为分散相的液溶胶称为悬浮液或悬浊液。固体悬浮的操作范围很广,颗粒的自由沉降速度为0.025~0.10m/s,而固体浓度可高达50%(质量分数)。  

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