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[OpenGL program] BLH DL : 0: 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
Update : 2025-02-19 Size : 152kb Publisher : 李光
[GPS develop] ecef2eci DL : 0: 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.
Update : 2025-02-19 Size : 2kb Publisher : 陈小摆
[MiddleWare] eci DL : 0: 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
Update : 2025-02-19 Size : 15kb Publisher : 王伟
[matlab] WGS84_target_to_earth_fix DL : 0: Latitude, longitude, altitude to earth ECI position conversion. WGS84 coordinates was used.-Latitude, longitude, altitude to earth ECI position conversion. WGS84 coordinates was used.
Update : 2025-02-19 Size : 1kb Publisher : David
[matlab] ECEFtoECI DL : 0: 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 frames is on the order of 1.2*10^-11 km when compared to STK ephemeris output.
Update : 2025-02-19 Size : 4kb Publisher : CYT
[ADO-ODBC] ECIFunctionTest DL : 0: 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
Update : 2025-02-19 Size : 2.39mb Publisher : 小蛮
[matlab] zuobiaoxizhuanhuan DL : 0: GPS中ECEF\LLW\ECI等坐标系的转换，为matlab程序，已打包-GPS ecef,eci,llw...
Update : 2025-02-19 Size : 7kb Publisher : yuhaiyu
[Algorithm] cppOrbitTools-test DL : 0: 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
Update : 2025-02-19 Size : 53kb Publisher : changlinglv
[Algorithm] David-Vallado DL : 2: 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.
Update : 2025-02-19 Size : 980kb Publisher : changlinglv
[Windows Develop] Teecef2ecih DL : 0: 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.
Update : 2025-02-19 Size : 2kb Publisher : zhengguoo
[Other] geo2eci.pro DL : 0: coordinate transformation code of IDL_from GEOGRAPHIC coordinate to ECI coordinate
Update : 2025-02-19 Size : 1kb Publisher : joannafaith
[Other] eci2geo.pro DL : 0: coordinate transformation code of IDL_from ECI coordinate to GEO coordinate
Update : 2025-02-19 Size : 1kb Publisher : joannafaith
[matlab] radar DL : 0: 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
Update : 2025-02-19 Size : 2kb Publisher : shuli
[matlab] J2Prop DL : 0: 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.
Update : 2025-02-19 Size : 1kb Publisher : 朱啸宇
[MPI] H1 DL : 0: 卫星轨道计算 ECI ECEF TOPO 坐标系以及相关输出函数等-satellite orbit
Update : 2025-02-19 Size : 404kb Publisher : Bowen Zhou
[source in ebook] ECI_ECEF DL : 0: 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)
Update : 2025-02-19 Size : 4kb Publisher : qwqwqwqwqw
[Other] ECItoECEF DL : 0: 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_ECEF] = ECItoECEF(JD,r_ECI,v_ECI,a_ECI); Where: JD is the Julian Date vector [1 x N] (units are in days) r_ECI is the position vector [3 x N] (any units are permitted) v_ECI is the velocity vector [3 x N] (any units are permitted) a_ECI is the acceleration vector [3 x N] (any units are permitted))
Update : 2025-02-19 Size : 1kb Publisher : ballackay