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Description: 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
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Size: 155648 |
Author: 李光 |
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Description: 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.
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Size: 2048 |
Author: 陈小摆 |
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Description: 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
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Size: 15360 |
Author: 王伟 |
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Description: Latitude, longitude, altitude to earth ECI position conversion. WGS84 coordinates was used.-Latitude, longitude, altitude to earth ECI position conversion. WGS84 coordinates was used.
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Size: 1024 |
Author: David |
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Description: 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.
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Size: 4096 |
Author: CYT |
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Description: 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
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Size: 2502656 |
Author: 小蛮 |
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Description: GPS中ECEF\LLW\ECI等坐标系的转换，为matlab程序，已打包-GPS ecef,eci,llw...
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Size: 7168 |
Author: yuhaiyu |
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Description: 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
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Size: 54272 |
Author: changlinglv |
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Description: 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.
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Size: 1003520 |
Author: changlinglv |
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Description: 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.
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Size: 2048 |
Author: zhengguoo |
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Description: coordinate transformation code of IDL_from GEOGRAPHIC coordinate to ECI coordinate
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Size: 1024 |
Author: joannafaith |
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Description: coordinate transformation code of IDL_from ECI coordinate to GEO coordinate
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Size: 1024 |
Author: joannafaith |
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Description: 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
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Size: 2048 |
Author: shuli |
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Description: 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.
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Size: 1024 |
Author: 朱啸宇 |
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Description: 卫星轨道计算 ECI ECEF TOPO 坐标系以及相关输出函数等-satellite orbit
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Size: 413696 |
Author: Bowen Zhou |
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Description: 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)
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Size: 4096 |
Author: qwqwqwqwqw |
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Description: 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))
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Size: 1024 |
Author: ballackay |
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