航天器轨道运算经常用到的函数我要分享

Functions often used in orbit calculation of spacecraft

matlab轨道计算 轨道-要素 ecef-eci 二体运动-matlab 轨道要素

关注次数: 450

下载次数: 3

文件大小: 18K

代码分类: 仿真计算

开发平台: matlab

下载需要积分: 1积分

版权声明:如果侵犯了您的权益请与我们联系,我们将在24小时内删除。

代码描述

中文说明:进行航天器轨道运算经常用到的函数,包括坐标转换,经纬度转换,二体运动,轨道要素计算等等


English Description:

The functions often used in orbit calculation of spacecraft include coordinate transformation, longitude and latitude conversion, two body motion, orbit element calculation and so on


代码预览

Orbital_compute

...............\CalcEA.m

...............\Constants.m

...............\dInc.m

...............\dVdI.m

...............\ecef2eci.m

...............\eci2ecef.m

...............\elorb.m

...............\Groundtrack.m

...............\Hohmann.m

...............\JD.m

...............\KeplerCOE.m

...............\NodeChange.m

...............\nuFromM.m

...............\nuFromTp.m

...............\plotorb.m

...............\R1.m

...............\R2.m

...............\R3.m

...............\randv.m

...............\RVtoLatLong.m

...............\topo.m

...............\TwoBody.m

...............\zeroTo360.m