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  1. ECEFtoECI

    3下载:
  2. 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
  3. 所属分类:matlab例程

    • 发布日期:2013-10-24
    • 文件大小:3760
    • 提供者:CYT
  1. exercise1

    2下载:
  2. 考虑章动、极移、岁差下历元时刻月球在瞬时平天球坐标系,J2000协议地固系,WGS-84坐标系下的位置速度矢量及转换的matlab源程序-Consider nutation, polar motion, precession next epoch in the instantaneous level of the moon celestial coordinate system, J2000 protocol to the solid line, the position and the vel
  3. 所属分类:matlab

    • 发布日期:2017-04-14
    • 文件大小:5567
    • 提供者:李涛
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