ECI2ECEF & ECEF2ECI Transformations (https://www.mathworks.com/matlabcentral/fileexchange/61957-eci2ecef-ecef2eci-transformations), MATLAB Central File Exchange. Retrieved September 28, 2024. MATLAB Release Compatibility Created with R2024a Compatible with any release Platform Compatibility Windows ...
这样的值是不太方便进行空间计算的，所以很多时候可以选取一个站心点，将这个很大的值变换成一个较小的...
The Influence of Application a Simplified Transformation Model Between Reference Frames ECEF and ECI onto Prediction Accuracy of Position and Velocity of G... In computational tasks of satellite geodesy there is a need for transformation of coordinates between reference frames ECEF – Earth Centered, ...
Because of the polar motion approximation that this reduction method uses, dcmeci2ecef calculates the transformation matrix rather than the direction cosine matrix. IAU-2000/2006 Reduce the calculation using the International Astronomical Union (IAU)-2000/2005 reference system. Choose this reduction ...
Currently, SatelliteToolbox.jl has functions to compute the rotation description (DCM or Quaternion) between the coordinate frames supported. Hence, you can represent the velocity in ECEF using the same matrix. However, I think that what you want is to change the time-derivative so that it is...
Krzyek RobertSkorupa BogdanReports on Geodesy and GeoinformaticsThe influence of application a simplified transformation model between reference frames ECEF and ECI onto prediction accuracy of position and velocity of GLONASS satellites. KRZYZEK R,SKORUPA B. Reports on Geodesy and Geoinformatics . 2015...
See Also dcmeci2ecef | ecef2lla | geoc2geod | geod2geoc | lla2ecef | lla2eciWhy did you choose this rating? Submit How useful was this information? Unrated 1 star 2 stars 3 stars 4 stars 5 stars × Select a Web Site Choose a web site to get translated content where available...
以图形学的观点来看，地心坐标可以看作是世界坐标，站心坐标可以看作局部坐标。
reduce the calculation. This model and theory are no longer current, but the software provides this reduction method for existing implementations. Because of the polar motion approximation that this reduction method uses,dcmeci2ecefcalculates the transformation matrix rather than the direction cosine ...
[r_eci] = ecef2eci(utc,r_ecef) calculates the position vector in the Earth-centered inertial (ECI) coordinate system for a given position vector in the Earth-centered Earth-fixed (ECEF) coordinate system at a specific Coordinated Universal Time (UTC). For more information on the Earth-cente...