1) interior ballistic equations
内弹道方程
1.
Aimed at the complexity and real law of loads on gun tube in the process of projectile lanuch,based on the interior ballistic equations,taken account of the flexible effect of gun tube,the dynamic coupling equations that describe the vibration response law were established.
针对火炮发射过程中身管受载的复杂性,以内弹道方程为基础,考虑发射过程中身管受载的实际规律,计及身管的柔性效应,建立描述身管振动响应规律的动力学方程组。
2) inner launch-trajectory equations
内弹道方程组
1.
The inner launch-trajectory equations and vapor-discharge equation for deck-landing aircrafts were established.
建立了舰载机弹射内弹道方程组和蒸汽流量方程,根据内弹道设计指标要求和飞机参数对弹射过程进行了仿真计算。
3) Trajectory Equation
弹道方程
1.
A mathematic model of using trajectory equations for firing data is presented.
给出了一种利用弹道方程决定射击诸元的数学模型 。
2.
Based on trajectory equation under the assumptions of the restricted two-body problem and neglect the effect of gravity on interceptor\'s and target\'s motion state,the linear function between the initial guidance errors and the terminal zero effort miss vector is proposed for space interception.
基于理想二体假设下的弹道方程解析式,忽略重力在拦截末段对拦截器和目标运动状态的影响,推导了空间拦截初始制导偏差与终端零控脱靶量之间的线性近似计算式,并以速度增量的大小来近似描述拦截末端主动寻的制导段的能量需求,给出了拦截末段制导最小能量需求与零控脱靶量、探测距离之间的近似关系。
4) interior ballistic process
内弹道过程
1.
The characteristics of develop- ment of the interior ballistic process has been derived.
首次给出了再生式液体发射药火炮中液注扩展、气相速度、气相压力和气相温度的时空分布规律，深入揭示了内弹道过程的发展特征。
5) trajectory equations
弹道方程组
1.
This paper presents an algorithm for finding projectile flight time with ensured acccuracy by solving the trajectory equations with unknown angle of departure only one time.
提出一种在保证一定计算精度的前提下，只解一次弹道方程组就可求得未知射角情况下目标点相应弹丸飞行时间的算法，而不需要在先求得准确射角后再解一次弹道方程组求解。
6) exterior trajectory equation
外弹道方程
补充资料：弹道(见弹道学)
弹道(见弹道学)
trajectory
dQfldQO弹道(t rajectory)见弹道学。
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