1) angle of trajectory rotation
弹道偏角
2) ballistic deflection
弹道偏差
1.
The reasons of deflection when the antitank missile is under lean firing were presented;and mathematical model of ballistic deflection was built to give quantitative analysis for ballistic deflection when the antitank missile lean firing.
论述某反坦克导弹侧倾射击时产生偏差的原因;通过受力分析和坐标系变换并经过推理运算,建立弹道偏差的数学模型,从而定量分析侧倾射击时某反坦克导弹的弹道偏差;结合射手训练的实际,给出侧倾射击时弹道偏差修正的具体操作及侧倾射击时的注意事项。
3) angle of flight path
弹道倾角
1.
At first the ballistic model of rocket projectile vertical launch is established,then it researches lift-to-drag ratio and influence of the angle of flight path on the firing range.
首先建立了火箭弹垂直发射的弹道模型,然后研究了升阻比、弹道倾角等参数的变化对火箭弹射程的影响,并分别对这两种情况进行了仿真。
4) flight-path angle
弹道角
5) ballistic windage deviation
弹道风偏差
6) deflect a bullet from its course
使子弹偏离弹道
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