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BLH
- 可以根据不同的椭球参数进行空间坐标系向大地坐标系的转换-Can be based on different parameters of the ellipsoid to the earth coordinate system of space coordinates conversion
ecef2eci
- 此matlab函数可以在ECEF和ECI坐标之中转换地点和速率信息。-This matlab function ECEF and ECI can convert the coordinates of the location and rate information.
eci
- 是IBM的CICS中间件上执行eci调用的样例，安装AIX5.3&CICS6.2后的官方例子-CICS is IBM' s middleware eci call on the implementation of the sample, after the installation of AIX5.3 & CICS6.2 official examples
WGS84_target_to_earth_fix
- Latitude, longitude, altitude to earth ECI position conversion. WGS84 coordinates was used.-Latitude, longitude, altitude to earth ECI position conversion. WGS84 coordinates was used.
ECEFtoECI
- Convert WGS 84 (CTS, ECEF) Coordinates to ECI (CIS, Epoch J2000.0) Coordinates. This function has been vectorized for speed. The associated error in converting between coordinate fr a mes is on the order of 1.2*10^-11 km
ECIFunctionTest
- 天津神舟通用数据技术有限公司神通数据库ECI函数使用demo-Universal Data Technology Co., Ltd. Tianjin Shenzhou supernatural database demo using the ECI function
zuobiaoxizhuanhuan
- GPS中ECEF\LLW\ECI等坐标系的转换，为matlab程序，已打包-GPS ecef,eci,llw...
cppOrbitTools-test
- 轨道计算，根据TlE轨道参数计算出ECI坐标等空间物体信息。-orbit computing
David-Vallado
- 通过NOARD的TLE参数进行轨道参数计算，得出ECI坐标等信息。-Through the NOARD TLE parameters of orbit parameters calculated, ECI coordinates and other information.
Teecef2ecih
- 此matlab函数可以在ECEF和ECI坐标之中转转换地点和速率信息。 ，经测试可直接使用。 -This Matlab function can be transferred into the ECEF and ECI coordinate conversion location and rate information. Has been tested and can be used directly.
geo2eci.pro
- coordinate transformation code of IDL_from GEOGRAPHIC coordinate to ECI coordinate
eci2geo.pro
- coordinate transformation code of IDL_from ECI coordinate to GEO coordinate
radar
- 航天器轨道力学 ECEF 地心地固系、东北天坐标系、ECI坐标转换 时间基准换算 轨道参数计算-Spacecraft orbital mechanics to EarthFixed ECEF system, northeast sky coordinates, ECI coordinate conversion parameter calculation time base conversion orbit
J2Prop
- 二体问题条件下，带有J2摄动的ECI状态量传播预测，-Propagate an ECI state into the future with the J2 perturbation.
H1
- 卫星轨道计算 ECI ECEF TOPO 坐标系以及相关输出函数等-satellite orbit
ECI_ECEF
- ECI与ECEF转换关系，卫星轨道模型方法，应用相关(ECI and ECEF conversion relation, satellite orbit model method, application correlation)
ECItoECEF
- 类似J2000的ECI坐标系转换到类似wgs84的ECEF坐标系,方便大家应用(Convert ECI (CIS, Epoch J2000.0) Coordinates to WGS 84 (CTS, ECEF) Coordinates. This function has been vectorized for speed. Example Function Call: >> [r_ECEF v_ECEF a_E