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#include <stdio.h> #include <math.h> #include "astro.h" #define EQtoECL 1 #define ECLtoEQ (-1) /* given the modified Julian date, mjd, and an equitorial ra and dec, each in * radians, find the corresponding geocentric ecliptic latitude, *lat, and * longititude, *lng, also each in radians. * correction for the effect on the angle of the obliquity due to nutation is * included. */ eq_ecl (mjd, ra, dec, lat, lng) double mjd, ra, dec; double *lat, *lng; { ecleq_aux (EQtoECL, mjd, ra, dec, lng, lat); } /* given the modified Julian date, mjd, and a geocentric ecliptic latitude, * *lat, and longititude, *lng, each in radians, find the corresponding * equitorial ra and dec, also each in radians. * correction for the effect on the angle of the obliquity due to nutation is * included. */ ecl_eq (mjd, lat, lng, ra, dec) double mjd, lat, lng; double *ra, *dec; { ecleq_aux (ECLtoEQ, mjd, lng, lat, ra, dec); } static ecleq_aux (sw, mjd, x, y, p, q) int sw; /* +1 for eq to ecliptic, -1 for vv. */ double mjd, x, y; /* sw==1: x==ra, y==dec. sw==-1: x==lng, y==lat. */ double *p, *q; /* sw==1: p==lng, q==lat. sw==-1: p==ra, q==dec. */ { static double lastmjd = -10000; /* last mjd calculated */ static double seps, ceps; /* sin and cos of mean obliquity */ double sx, cx, sy, cy, ty; if (mjd != lastmjd) { double eps; double deps, dpsi; obliquity (mjd, &eps); /* mean obliquity for date */ nutation (mjd, &deps, &dpsi); eps += deps; seps = sin(eps); ceps = cos(eps); lastmjd = mjd; } sy = sin(y); cy = cos(y); /* always non-negative */ if (fabs(cy)<1e-20) cy = 1e-20; /* insure > 0 */ ty = sy/cy; cx = cos(x); sx = sin(x); *q = asin((sy*ceps)-(cy*seps*sx*sw)); *p = atan(((sx*ceps)+(ty*seps*sw))/cx); if (cx<0) *p += PI; /* account for atan quad ambiguity */ range (p, 2*PI); }
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