201700202004于瑞
代码说明：
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
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