在SHEL的最初测试中，ABL飞机使用安装在“大乌鸦”飞机上的激光信标模拟实际导弹目标会产生的返回信号。
On this initial test of the SHEL, ABL made use of beacon lasers installed on Big Crow to simulate the targeting return it would receive from a live missile target.
在演习时，我们链接导弹防御指挥和控制系统，这是北约已开发的真实和模拟传感器，以练习对抗威胁的能力。
During the exercise, the NATO Active Layered Theatre Ballistic Missile Defence Programme underwent a series of important tests, prior to its handover to NATO commanders. "During."
这种模拟器将被用来判断海军和海军陆战队飞机的对抗系统的能力，飞机的对抗系统用来保护飞机免受敌方导弹的威胁。
The simulator will be used to determine the effectiveness of Navy and Marine Corps aircraft countermeasure systems that protect the aircraft from hostile missiles.
介绍了为实现电子模拟运算导弹允许发射距离的数学模型，并说明了雷达距离比例尺的变换方法。
This paper introduce the mathematical model to realize the electronic analog computation to missile allowable launching distance and explain the transforming way of radar range scale.
采用以N-S方程为主控方程的数值模拟方法，进行固定尾翼鸭式气动布局导弹的气动特性和流场数值模拟。
To investigate the rolling control characteristics of canard-controlled missile with fixed-tail, a numerical simulation method based on N-S formulation was conducted.
从作战模拟和效能评估的角度出发，建立了反辐射导弹(ARM)导引头的截获模型、跟踪模型和ARM的雷达截面积模型。
An interception model, a tracking model of the ARM seeker and a RCS model of the ARM are founded based on the need of combat simulations and effectiveness evaluation.
掠海导弹飞行模拟靶标是完成近程反导舰炮武器系统研制试验及装备交验所必须的重要靶标之一。
Flying simulated drone of skimming sea missile is one of the important drone to complete short range antimissile warship gun weapon system development test and equipment adopt.
介绍了便携式防空导弹双色导引头中所采用的数字式控制系统代替传统的模拟式控制系统的方法。
Introducing the method for replacing traditional simulating control systems with a digital one in the dual-mode seeker of, portable air defense missiled. Simplifying.
本文对研究导弹系统模拟打靶的蒙特卡洛法与统计协方差法进行分析、比较。
This paper presents the analysis and comparison between Monte carlo method and statistical covariance method which are used to research analog target of missile system.
许多计算机持续运转，模拟预测在战时导弹失败的可能性或在和平时期导弹惹祸的恶果。
Computers are constantly running simulations to predict the likelihood of missile failure in a war, or the consequences of a missile mishap while still in peacetime.
考虑了对机动导弹实施机动区域打击，建立起在圆环形区域瞄准点选取模型，并通过计算机模拟进行了结果分析。
Attacking the mobile missile base is considered and an aim-point-choosing model for striking its ring mobile region is presented. The simulation model is realized and the result is analyzed.
该方法简洁实用，而且使用先进的快速模拟法计算导弹允许攻击区，使计算速度大大提高。
The method is concise and practical, and uses advanced "fast simulation method" to calculate missile launch boundary which makes calculating velocity much faster.
采用多块嵌套结构动网格技术数值模拟了拦截导弹的热保护罩的二维分离过程。
Two-dimensional simulations about the separation of the interceptor missile shroud covers have been completed using moving multi-block chimera structure grid technique.
为了降低便携式地空导弹射击训练器材的生产成本并提高其使用寿命，提出了一种用模拟导引头替代机械陀螺导引头设计方法。
In order to reduce the cost and increase the life of portable surface-to-air missile weapon training equipment, it is put forward to use a simulative seeker to replace mechanical gyro seeker.
针对导弹武器系统模拟测试方案存在的不足，提出了基于现场总线的数字化测试方案，文中从硬件和软件方面给出了惯性测量组合测试节点与 CAN 总线的接口设计。
We put forword one Check-up and control system based on CAN-bus, and introduced its whole structure, hardware collocation, software Collocation, interface-circuit and so on.
针对导弹武器系统模拟测试方案存在的不足，提出了基于现场总线的数字化测试方案，文中从硬件和软件方面给出了惯性测量组合测试节点与 CAN 总线的接口设计。
We put forword one Check-up and control system based on CAN-bus, and introduced its whole structure, hardware collocation, software Collocation, interface-circuit and so on.
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