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/dports/astro/py-ephem/ephem-4.1.3/libastro/
H A Dearthsat.c53 double Eccentricity, double RAANPrecession, double PerigeePrecession,
75 double Inclination, double *RAANPrecession, double *PerigeePrecession);
279 double RAANPrecession,PerigeePrecession; in esat_prop() local
293 GetPrecession(SemiMajorAxis,Eccentricity,Inclination,&RAANPrecession, in esat_prop()
313 Inclination,Eccentricity,RAANPrecession,PerigeePrecession, in esat_prop()
320 printf ("RAANPrecession = %g\n", RAANPrecession); in esat_prop()
545 double *RAANPrecession, double *PerigeePrecession) in GetPrecession() argument
547 *RAANPrecession = 9.95*pow(EarthRadius/SemiMajorAxis,3.5) * cos(Inclination) in GetPrecession()
564 double RAANPrecession, double PerigeePrecession, double T, in GetSatPosition() argument
594 RAAN = EpochRAAN - (T-EpochTime)*RAANPrecession; in GetSatPosition()