... 弹道火箭 ballistic vehicle 弹道计算 trajectory computation 弹道降落距离 drop ...
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Further, a simulation system is designed in order to virtually simulate the process of missile interception. Three linked computers are brought in, and trajectory calculation, data exchange and demo programs are designed.
为了模拟导弹拦截过程,本文还设计了一套仿真系统,采用了三机联合仿真的方式,并逐一介绍了弹道计算程序、数据交互程序和动画演示程序的设计思路。
参考来源 - 拦截弹的导引规律研究与仿真·2,447,543篇论文数据，部分数据来源于NoteExpress
分析燃气蒸气式发射动力系统内弹道计算产生误差的影响因素。
This paper analyzed the influencing factors of errors of interior ballistic calculation in gas and steam type launch power system.
在内弹道计算中，设燃烧产物为准定常流动，使用分段解析法进行内弹道的数值模拟。
The numerical simulation was carried out to compute internal ballistics by segmented analytical method in the assumption of grains steady flow of burning product.
此动力学模型可用于弹丸大攻角飞行时的弹道计算及某些灵巧弹药（如末敏弹）的设计。
This kinetic model can be used in ballistic calculation of projectile with large angle of attack and also in the design of some smart munitions(e. g. target sensitivity projectile).
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