英德
有道
百度
谷歌
图片
维基
百科
弹道倾角
trajectory inclination angle
- 设计了以再入飞行器落点偏差和飞行高度为输入，弹道倾角角速度为输出的模糊逻辑系统；
The system of fuzzy logic was designed with altitude and deviation on target as system inputs and the angular rate of flight path angle as system output. - 根据惯导、高度表和雷达提供的信息，设计了以弹道倾角为被控对象的导引规律，实现了以上目标。
Based on the information obtained from INS, altimeter and radar, the guidance law with trajectory inclination angle as its controlled output is designed to achieve the above goal. - 为保证飞航导弹末段的突防效果，提高战斗部的杀伤威力，要求导弹在末段进行跃起俯冲并以一定的弹道倾角命中目标。
In order to guarantee terminal penetration effect and raise warhead's lethality, cruise missile should take jump-dive maneuver and obtain specific incident angle to hit the target.
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