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.- 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.