文件名称:proportional-guidance-law
-
所属分类:
- 标签属性:
- 上传时间:2013-06-04
-
文件大小:661.62kb
-
已下载:2次
-
提 供 者:
-
相关连接:无下载说明:别用迅雷下载,失败请重下,重下不扣分!
介绍说明--下载内容来自于网络,使用问题请自行百度
介绍了比例导引法的导引规律,推导了基于比例导引规律的拦截弹弹道方程.给出了一种目标做正弦
机动飞行的轨道方程,并采用Matlab对拦截弹拦截目标进行了目标拦截仿真.分析了拦截弹速度和目标速度,以
及导引系数对拦截弹弹道的影响,研究了导弹实际飞行中弹道曲率与法向过载的关系.-Proportional guidance law is introduced,and trajectory equation of intercepting missile based
on proportional guidance law is deduced.A kind of orbit equation of target in sine mobility is given,and
the missile intercepting the target is simulated with Matlab.The influence of missile speed,target speed
and guidance mode on the trajectory is analyzed.The relationship between trajectory curvature and normal
over-loading is researched.
机动飞行的轨道方程,并采用Matlab对拦截弹拦截目标进行了目标拦截仿真.分析了拦截弹速度和目标速度,以
及导引系数对拦截弹弹道的影响,研究了导弹实际飞行中弹道曲率与法向过载的关系.-Proportional guidance law is introduced,and trajectory equation of intercepting missile based
on proportional guidance law is deduced.A kind of orbit equation of target in sine mobility is given,and
the missile intercepting the target is simulated with Matlab.The influence of missile speed,target speed
and guidance mode on the trajectory is analyzed.The relationship between trajectory curvature and normal
over-loading is researched.
(系统自动生成,下载前可以参看下载内容)
下载文件列表
旭橥Matlab钴蒿智?熠????萋喟.pdf
proportional guidance law.pdf
proportional guidance law.pdf
本网站为编程资源及源代码搜集、介绍的搜索网站,版权归原作者所有! 粤ICP备11031372号
1999-2046 搜珍网 All Rights Reserved.