Kepler_orbit_rotate
所属分类:matlab编程
开发工具:matlab
文件大小:3KB
下载次数:122
上传日期:2010-03-08 10:55:07
上 传 者:
hailanchao
说明: 计算得出导弹的被动段飞行轨迹(未考虑大气)和再入点、落点信息(在发射惯性坐标系内的位置量)
(Calculated the passive missile flight path segment (not to consider the atmosphere) and re-entry point, placement of information (in the firing position within the inertial coordinate system volume))
文件列表:
Kepler_orbit_rotate.m (6547, 2006-06-15)
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