Description: ALM2POS computation for satellite position from almanac data file
[pos,R]=alm2pos(almanac,PRN,time) calculates the satellite position in the
Terrestial and in the Celestial reference frame for a desiderate satellite
vehicle (PRN) with almanac data (ALMANAC). The given time (TIME) can be a
scalar or also a vector. Colomn 1-3 of position (pos) are Terrestial
Coordinates (ECEF) colomn 4-6 of position are Celestial Coordinates (ECSF)
in m. Another output is the position vector of the satellite (R) in m.
- [Pmode] - According to the principle of p-code gen
- [alm2skyplot] - ALM2SKYPLOT is a program for the satell
- [skyplot] - SKYPLOT for a given receiver position Y
- [GioveAB_Orbit_Simulator] - The actual version requires the followin
- [codegen] - GPS signal generated C/A code of the MAT
- [ReadNavFile] - Read broadcast star calendar，Calculate t
File list (Check if you may need any files):
alm2pos.m
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