201700202004于瑞
所属分类：matlab编程
开发工具：matlab
文件大小：1774KB
下载次数：2
上传日期：2020-10-26 16:58:30
上 传 者：
lianhe12
说明： 仿真卫星轨道，输出轨道六根数，完成赤道天球坐标系到地心固连坐标系的转换
(Simulation of satellite orbit, output six orbital elements, complete the transformation from equatorial celestial coordinate system to earth center fixed coordinate system)
文件列表:
201700202004于瑞\a4xiugai.m (3808, 2019-12-21)
201700202004于瑞\Angle0_2pi.m (514, 2019-09-27)
201700202004于瑞\Date2Mjd.m (940, 2019-09-25)
201700202004于瑞\ECI2ECF.m (907, 2019-09-29)
201700202004于瑞\Figure1.fig (446039, 2019-10-19)
201700202004于瑞\figure2.fig (558008, 2019-10-19)
201700202004于瑞\fugaidai.m (1046, 2019-12-21)
201700202004于瑞\main2.m (3304, 2019-10-19)
201700202004于瑞\Mjd2Date.m (1421, 2019-09-25)
201700202004于瑞\qiuguidaogenshu.m (685, 2019-10-19)
201700202004于瑞\qiu_g_r_v.m (639, 2019-10-19)
201700202004于瑞\sataborbit.dat (797074, 2019-10-19)
201700202004于瑞\sataborbit.txt (797074, 2019-10-19)
201700202004于瑞\空天飞行力学项目中期报告.docx (492174, 2019-10-19)
201700202004于瑞 (0, 2020-03-24)
近期下载者：
相关文件：
收藏者：