2) Laser beam riding guidance
激光驾束制导
1.
In order to test laser beam riding guidance information field,this paper introduces the design scheme and principle of the testing system in detail according to parameters of information field.
为了完成激光驾束制导信息场检测,根据信息场的参数,介绍了检测系统的设计方案和工作原理;基于误差设计理论,根据激光束传输特性,利用光学软件ZEMAX设计了激光信息场检测光学系统;通过信息场指令值和辐照度检测,实现信息场参数测试。
3) anti-tank missile
反坦克导弹
1.
General hierarchy and basic method of the efficiency evaluation of vehicular anti-tank missile weapon system are discussed at length.
详细探讨了车载反坦克导弹武器系统效能评估的总体层次结构和基本方法,建立了系统效能评估模型,在此基础上,构建了系统效能评估仿真软件,并以某反坦克导弹武器系统为例进行了系统效能仿真评估,为缩短反坦克导弹武器的研制周期,提高其效费比以及整体作战效能提供了理论参考。
2.
Aiming at the phenomenon of anti-tank missile can not hit the goal after the missile launched,the failure mode that the missile falls down in short distance,flies high in long distance and undershoot were studied,and then the failure mode was presented.
针对反坦克导弹发射后不中目标的现象,采用故障树分析法对近距离掉弹、远距离高飞和脱靶的一般故障模式进行了研究,并给出了一般故障弹模式。
3.
The indoor launching characteristics of anti-tank missile and the possibility of injury to firers were analyzed systematically.
系统分析了反坦克导弹室内射击的特点、可能对射手造成的损伤,通过试验重点分析便携式反坦克导弹在以房舍为代表的狭小空间内射击时物理和化学环境变化对生物的影响,为便携式反坦克导弹适应房舍等狭小工事内射击的设计和使用提供参考依据。
4) antitank missile
反坦克导弹
1.
The reasons of deflection when the antitank missile is under lean firing were presented;and mathematical model of ballistic deflection was built to give quantitative analysis for ballistic deflection when the antitank missile lean firing.
论述某反坦克导弹侧倾射击时产生偏差的原因;通过受力分析和坐标系变换并经过推理运算,建立弹道偏差的数学模型,从而定量分析侧倾射击时某反坦克导弹的弹道偏差;结合射手训练的实际,给出侧倾射击时弹道偏差修正的具体操作及侧倾射击时的注意事项。
2.
Based on the aerodynamic configuration of New Javelin light antitank missile, a series of wind tunnel experimental model was designed with the component build-up method.
以美国的“新标枪”轻型反坦克导弹外形为基础,采用部件组合法设计一组风洞实验模型,进行六分量测力实验,实验马赫数范围为0·3~0·5,攻角范围为-1°~15°。
3.
According to the general program of a portable antitank missile steering to hit on top of the tank at terminal trajectory, this paper presented the closed-loop control stiffness ballistic model and simulation for the straight flight, the glancing flight and terminal steering trajectory under both the fixed and active targets.
在末端姿态弹体折转控制、掠飞击顶轻型反坦克导弹总体方案论证的基础上 ,利用某反坦克导弹的总体参数 ,建立了这种新型导弹的闭环控制刚体弹道模型 ,进行了固定目标平飞、固定和活动目标掠飞折转等三种闭环控制弹道的全数字仿真 ,仿真结果表明 ,末端姿态弹体折转控制击顶的总体方案技术可
5) ATGM(antitank guided missile)
[军]反坦克制导导弹
补充资料:上驾
1.指优等马。 2.帝王的车驾。借指帝王。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
参考词条