1) 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。
2) 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。
3) 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。
4) exterior trajectory equation
外弹道方程
5) equations of point-mass trajectory
质点弹道方程组
6) relative trajectory equation
相对弹道方程
1.
By combining the differential equation with the according guidance law, a relative trajectory equation is set up which will help to study the characteristic of trajectory.
在传统的动力学微分方程的基础上提出了一种扩展的比例导引法 ,并给出了该导引规律下的相对弹道方程。
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