ocssw
V2022
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Go to the source code of this file.
Functions | |
void | ephparms (double t, double *xls, double *gs, double *xlm, double *omega) |
Function Documentation
◆ ephparms()
void ephparms | ( | double | t, |
double * | xls, | ||
double * | gs, | ||
double * | xlm, | ||
double * | omega | ||
) |
This subroutine computes ephemeris parameters used by other Mission Operations routines: the solar mean longitude and mean anomaly, and the lunar mean longitude and mean ascending node. It uses the model referenced in The Astronomical Almanac for 1984, Section S (Supplement) and documented and documented in "Exact closed-form geolocation algorithm for Earth survey sensors", by F.S. Patt and W.W. Gregg, Int. Journal of Remote Sensing, 1993. These parameters are used to compute the solar longitude and the nutation in longitude and obliquity.
- Parameters
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t Time in days since January 1, 2000 at 12 hours UT xls Mean solar longitude (degrees) gs Mean solar anomaly (degrees) xlm Mean lunar longitude (degrees) omega Ascending node of mean lunar orbit (degrees)
Definition at line 3 of file ephparms.c.