trajectory-controlled meaning in English
弹道可控的
Examples
- At present , the most effective method of destroying the warhead of btm is the technology of directly hit kinetic kill , which can achieve precision control to the missile by adding the trajectory - control jet or attitude - control jet
目前对付来袭tbm弹头最有效的手段就是采用直接碰撞动能杀伤技术。它是通过在导弹上安装响应快速的双组元轨、姿控发动机以实现对导弹的精确控制。 - The main works and achievements are described : ( 1 ) the application of direct lateral force on the exoatmosphere kinetic - kill vehicle . at first , the collectivity project of the exoatmosphere kinetic - kill vehicle is specified , the motive model of the exoatmosphere kinetic - kill vehicle and target are constructed , and the thrust performance of trajectory - control engine and attitude - control engine are presented
研究的内容及成果主要表现在以下几个方面： (一)直接侧向力在大气层外动能拦截器中的应用首先确定了动能拦截器的总体方案，分别建立目标运动和动能拦截器运动的数学模型，以及轨控和姿控发动机的推力模型。 - The main work and achievements are described as follows : ( 1 ) the analysis of the extra - atmospheric kinetic - kill vehicle at first , the motion model and dynamics model of the kinetic - kill vehicle is constructed , and the thrust performance of trajectory - control system and attitude - control system are presented , then the algorithms of realizing the guidance law , the methods of trajectory and attitude control are studied
研究内容及成果主要表现在以下几个方面： (一)大气层外动能拦截器分析首先建立了动能拦截器运动学和动力学模型，以及轨控发动机和姿控发动机的推力模型，提出了拦截导引律的实现方法及轨控和姿控发动机的控制规律。 - The main works of this thesis are research of lateral force control and guidance of interceptors , emphasized on the terminal phase when intercepting the tactical ballistic missiles , including the performance analysis of extra - atmospheric kinetic - kill vehicle piloted by trajectory - control and attitude - control systems , and combined control of aerodynamics with lateral jets in atmosphere
本文主要研究拦截弹在拦截战术弹道导弹时，末段的制导和侧向力控制问题，包括大气层外动能拦截器在姿控与轨控发动机作用下的性能分析，和大气层内侧向力与气动力复合控制研究。 - And then based on a surface - to - air missile that satisfies the requisition nearly , by means of reconstructing its geometry size , subsystems such as engine , the interceptor model used to continue the following studies is established . then the trajectory - control jet or attitude - control jet is added to the interceptor based on the analysis of the relationship between the missile performance and the thrust and configuration of the side jet
然后以基本满足方案要求的某型防空导弹为基础，对其几何尺寸、发动机等分系统进行改进，并通过分析导弹性能与侧喷发动机参数之间的关系，增加了姿控或轨控侧向装置，这样得到了本文的研究工作所需的导弹模型。