1) terminal correction
末修
1.
The terminal correction submunition missile has good shooting efficiency when attacking the airdrome runway.
将机场跑道看作线目标,用末修子母弹对其攻击具有较高的射击效能。
2.
In this paper,the shooting efficiency for terminal correction sub-munition to airport runway is calculated by three methods:Monte-Carlo method,Numerical Value simulation method and CADET.
文中以某末修子母弹攻击机场跑道为例,用统计试验法、数值模拟法以及 CADET 三种方法计算了末修子母弹对机场跑道的射击效能。
3.
In this paper, according to sub munition’s flying characters and work theory of terminal detection and terminal correction parts, a new method of calculating the shooting probability of terminal correction sub munition is presented.
根据末修子弹的运动特点以及末敏、末修部件的工作原理 ,用近似的方法计算出子弹对机场跑道的探测概率 。
2) terminal correction
末段修正
1.
The paper puts forward a design scheme of simple impulse correction for terminal correction rockets,and establishes the model of corrected trajectory.
提出了一种末段修正火箭弹简易脉冲修正技术的设计方案,并建立了修正弹道模型。
2.
In view of the problem of correction of the end of ballistic trajectory of mortar,this paper builds a dynamics model based on impulse control and analyzes the effect of impulse and trajectory parameters on terminal correction ability and trajectory characteristic.
结合弹道模型,分析了脉冲个数、脉冲力大小、布置位置、弹丸转速、脉冲作用时间等脉冲参数和弹道参数对末段修正能力和弹道特性的影响规律。
3.
Impulse correction scheme of a terminal correction rocket was put forward,and the trajectory model was established.
提出了一种末段修正火箭弹的脉冲修正方案,建立了相应的弹道模型;对单个脉冲发动机的修正能力及修正时机进行了仿真研究;提出了末段多级修正的方法,并对多级修正进行了弹道数字仿真。
3) terminal correction projectile
末修弹
1.
The influential factors of the trajectory correction including the pulse motor starting control time,pulse motor quantity were analyzed and the application and limit of trajectory tracking used in terminal correction projectile were studied.
分析了脉冲启控时间、脉冲个数对修正效果的影响,并对弹道追踪导引律在末修弹中应用条件及其局限性进行了详细研究。
4) powder choiceness
粉末精修
5) Terminal correctional technology +
末修技术
6) velocity revision and attitude control in the final powered phase
末修姿控
补充资料：笃笃末末
1.盘盘旋旋。
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