English translation for "trajectory simulation"

飞行轨迹模拟

Related Translations:

trajectory:  n.(抛射体的)轨道，弹道；流轨；【几】轨线。 a curved [direct-fire, flat, highangle fire, low] trajectory 曲射[直射、平射、高射、低射]弹道。

ejection trajectory:  弹射轨迹

lofted trajectory:  过高弹道

selenocentric trajectory:  月心轨迹

return trajectory:  返回轨道

predicted trajectory:  预计弹道

actual trajectory:  实际弹道实际轨迹

trajectory dispersion:  偏离设计轨迹

computed trajectory:  计算弹道

trajectory height:  弹道高

Example Sentences:

	1.	Frame - oriented method on trajectory simulation 面向框架的弹道仿真方法
	2.	Missile trajectory simulation based on increment proportional guide 增量比例导引弹道仿真研究
	3.	Research on the whole flying trajectory simulation system of command guided antiaircraft missile 指令制导防空导弹全弹道飞行仿真系统研究
	4.	As combat simulation frame and as missile trajectory simulation model are setup in the paper 建立了空地作战任务仿真框架和空地导弹的弹道计算模型。
	5.	Analyzing to a stand off missile ' s flight characteristics , the as missile trajectory simulation is completed 在分析了典型防区外导弹飞行特点的基础上，进行空地导弹弹道仿真。
	6.	Abstract : the digital simulation methods for maintaining the trajectory on a given manifold are presented . particularly , the norm conserving schemes are given for the solution of the system of the quaternion equations in the trajectory simulation of the vehicle 文摘:给出保持轨道在给定流形上的数字仿真方法，特别对飞行器轨道仿真中的四元数微分方程组的求解给出保范处理。
	7.	Then we analyzed the change process of trajectory in air - to - ground missile attack , built the movement equations based on the center of gravity of every segment . in the end we gave the whole trajectory simulation result of air - to - ground attack 分析了空地导弹攻击的弹道变化过程，将攻击过程划分为五部分，分别对各段建立了重心运动方程并进行了仿真，最后给出了空地导弹攻击的全过程弹道仿真结果。
	8.	In this paper . the question of compound guidance about mid - long range air - to - air missle to be considered . the main contributions are as follows : first , two midcourse guidance laws are given . that is optimally predictable pn micourse guidance , which is suitable for middle range missle , and singularly perturbed midcourse guidance . which is suitable for long range missle guidance ; then two terminal guidance laws are given . that is variable structure guidance , which is suitable for passive radar guidance . and optimal guidance which is suitable for active radar guidance ; and then the error sourses of hand - off are researched , the hand - off law is given at the time ; fmally , the midcourse guidance laws and terminal guidance laws are tested by simulation , and the whole trajectory simulation are given through hand - off law , and the results are satisfied 主要工作如下：首先研究了用于中远程空空导弹复合制导的两种中制导律，即用于中程导弹的最优预测比例导引中制导律和用于远程导弹的奇异摄动中制导律，它们均有很好的中制导性能，能够满足中末制导的交班要求；接着研究了两种末制导律，即用于被动雷达末制导的变结构制导律和用于主动雷达导引头的最优末制导律，均适用于复合制导末制导段；然后分析了中末制导的交班误差源，讨论了用于复合制导的交接律；最后通过仿真，验证了提出的中制导律和末制导律，结合提出的交接规律，在不同的情况下对中末制导段弹道进行了仿真验证，结果证明文中提到的中末制导律能够达到性能指标要求。

Similar Words：

"trajectory peak" English translation, "trajectory prediction" English translation, "trajectory profile" English translation, "trajectory shaping" English translation, "trajectory shift" English translation, "trajectory slope angle" English translation, "trajectory techniques" English translation, "trajectory test" English translation, "trajectory test of depth charge" English translation, "trajectory vertex" English translation