Chinese translation for "导弹模型"

missile mockup
missile model
missile simulator

Related Translations:

面面导弹:  surface-to-surface missile

惯性导弹:  inertial missile

导弹周刊:  missile week

导弹方位:  missile bearing

子导弹:  daughter missilesub-projectile

靶标导弹:  target missile

导弹针:  a pin missile

导弹系统:  gmsguided-missile systemmissile system

攻击导弹:  offensive missile

面对面导弹:  ssmsurface-to-surface missile

Example Sentences:

	1.	At first , the rolling missile model had been established by referring to the figuration dimension of pac - 3 首先以“爱国者? 3 ”的外形尺寸为参考建立本文的研究工作所需的导弹模型。
	2.	The thesis tracks the research about the intercept technology oversea . the rolling missile model with attitude - control - system is established by referring to the figuration dimension of pac - 3 本文跟踪国外研究，以“爱国者? 3 ”导弹外形尺寸为参考建立了具有姿态控制系统的滚转导弹模型。
	3.	Meanwhile we research - ? filter , kalman filter and extend kalman filter . based on the requirement of gbr simulation system , we adopt extend kalman filter algorithm of ballistic missile model 对当前常用的滤波算法- ?滤波器、 kalman滤波器以及推广kalman算法进行了研究,并结合本仿真系统的特点,选择了使用弹道导弹模型的推广kalman滤波算法。
	4.	The proposed combined method can save time and enhance efficiency . the numerical results of some benchmark targets such cylinder , cone , missile model are given in this paper , they agree very well with the measurements or the results from general mom 本文给出了目标如圆柱体、圆锥体、导弹模型等运用这两种方法的结合后计算所得的单站rcs结果,这些结果均与测量值或者与用一般矩量法所得到的结果吻合。
	5.	C . based on a lot of referenced documents and tunnel experiment data , the phenomenon of lateral jet interception are analyzed , and the diagrams of the interaction factor " kcn " is presented . following , the airdefence missile model , trajectory model including attitude - control direct lateral force are constructed 3 、根据大量参考文献和试验数据，分析了侧向喷流的干扰特性，并给出不同状况下干扰因子k _ ( cn )的变化曲线，在上述工作的基础上，建立了带有姿控侧向力装置的防空导弹模型和弹道计算模型。
	6.	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。

Similar Words：

"导弹瞄准点" Chinese translation, "导弹瞄准台" Chinese translation, "导弹命中点" Chinese translation, "导弹命中目标" Chinese translation, "导弹模拟" Chinese translation, "导弹目标" Chinese translation, "导弹暖机时间" Chinese translation, "导弹排气流" Chinese translation, "导弹配置" Chinese translation, "导弹喷射流" Chinese translation