1)  angle of attack
命中角
1.
Target-ship is predigest as ellipsoid in this paper,on this condition,the calculative model of miss distance is established during torpedo tracking the target,the method of calculate angle of attack is given.
为了进行精确制导仿真,文中将目标体视为椭球体的几何体目标,建立了鱼雷攻击目标的脱靶量和命中角等命中要素的计算模型,并采用蒙特卡罗法进行统计仿真试验,得到命中概率、脱靶量均值、均方差、置信区间等统计结果。
2)  hitting target
命中
1.
Based on analyzing the principles of tank fire control system,the evaluation model for hitting target of tank firing training is established and tested in experiments.
对坦克实车射击过程及射击误差进行了分析,在对坦克火控系统原理进行分析的基础上,建立了射击命中评判模型,并进行了试验检验,实现了坦克实车嵌入式不装实弹进行射击训练的命中点评判。
3)  hit rate
命中率
1.
This paper analyzes the technological factors which might influence hit rate.
本文分析了影响投篮命中率的各种技术因素,并提出了相应的提高命中率的方法,为篮球教学工作提供有益的参考。
2.
A Web cache-cluster system with higher throughput and hit rate was proposed.
设计并实现一个具有较高吞吐率和命中率的Webcache机群缓存系统。
3.
The authors discuss in detail how to construct a native resource mechanism for improving the hit rate of fetching data from the server side.
本文介绍了在交互式网络数据库应用程序的开发中利用多线程方式提高客户端实时响应能力的解决方案,并着重讨论了如何合理地构造本地资源机制,以提高在客户端取数据时的命中率;最后还介绍了一个采用Java多线程的解决方案的具体实例,以及Java中线程间的调度问题。
4)  hit probability
命中概率
1.
We establish a model of torpedo hit probability under pure evasive maneuver situation by analyzing the organization of search area of two torpedoes salvo,possible target position area,selection of salvo aiming point,and the submarine evasive maneuver model.
通过对双雷齐射搜索面的组织、目标可能位置区域、齐射射击瞄准点的选取以及潜艇规避机动模型的分析,建立了潜艇纯机动规避情况下鱼雷命中概率仿真模型。
2.
Based on the characteristic of awaiting fire in the fire control theory,the problem of period hit probability to a maneuver target with properties of randomly passing through shot area was studied,that is,many hit probability under the condition of shooting time limited.
基于火控理论中待机射击的特点,研究了具有随机特性的机动目标随机穿越射击域时的周期命中概率问题,即穿越周期内射击时间受限条件下的多发命中概率。
3.
Because of the earth curvature,target data need to be detected by the friend unit and sent to ship,but data errors affect the hit probability.
远程化是反舰导弹的一个发展方向,由于地球曲率的影响,水面舰艇需依靠友方指示目标,目标指示数据的精度影响反舰导弹的命中概率。
5)  hit space
命中间隔
6)  hit error
命中误差
1.
After-working impulse is main source to ballistic missile flight trajectory error and hit error.
后效冲量误差是引起弹道导弹飞行弹道误差和命中误差的一个重要误差源。
参考词条
补充资料:定风波 商角调 商角调 西江客舍
【诗文】:
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