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- #include "sky.h"
-
- sat()
- {
- double pturbl, pturbb, pturbr;
- double lograd;
- double dele, enom, vnom, nd, sl;
- double q0, v0, t0, j0, s0;
-
- double capj, capn, eye, comg, omg;
- double sb, su, cu, u, b, up;
- double sd, ca, sa;
-
- object = "Saturn ";
-
- ecc = .0558900 - .000347*capt;
- incl = 2.49256 - .0044*capt;
- node = 112.78364 + .87306*capt;
- argp = 91.08897 + 1.95917*capt;
- mrad = 9.538843;
- anom = 175.47630 + .03345972*eday - .56527*capt;
- motion = 120.4550/3600.;
-
- q0 = 102.28 + 4.092334429*eday;
- q0 *= radian;
- v0 = 212.536 + 1.602126105*eday;
- v0 *= radian;
- t0 = -1.45 + .985604737*eday;
- t0 *= radian;
- j0 = 225.36 + .083086735*eday;
- j0 *= radian;
- s0 = 175.68 + .033455441*eday;
- s0 *= radian;
-
- anom = anom;
- incl *= radian;
- node *= radian;
- argp *= radian;
- anom = fmod(anom,360.)*radian;
-
- enom = anom + ecc*sin(anom);
- do {
- dele = (anom - enom + ecc * sin(enom)) /
- (1. - ecc*cos(enom));
- enom += dele;
- } while(fabs(dele) > 1.e-8);
- vnom = 2.*atan2(sqrt((1.+ecc)/(1.-ecc))*sin(enom/2.),
- cos(enom/2.));
- rad = mrad*(1. - ecc*cos(enom));
-
- lambda = vnom + argp;
-
- pturbl = 0.;
-
- lambda += pturbl*radsec;
-
- pturbb = 0.;
-
- pturbr = 0.;
-
- /*
- * reduce to the ecliptic
- */
-
- nd = lambda - node;
- lambda = node + atan2(sin(nd)*cos(incl),cos(nd));
-
- sl = sin(incl)*sin(nd) + pturbb*radsec;
- beta = atan2(sl, sqrt(1.-sl*sl));
-
- lograd = pturbr*2.30258509;
- rad *= 1. + lograd;
-
-
- lambda -= 1185.*radsec;
- beta -= 51.*radsec;
-
- motion *= radian*mrad*mrad/(rad*rad);
- semi = 83.33;
-
- /*
- * here begins the computation of magnitude
- * first find the geocentric equatorial coordinates of Saturn
- */
-
- sd = rad*(cos(beta)*sin(lambda)*sin(obliq) +
- sin(beta)*cos(obliq));
- sa = rad*(cos(beta)*sin(lambda)*cos(obliq) -
- sin(beta)*sin(obliq));
- ca = rad*cos(beta)*cos(lambda);
- sd += zms;
- sa += yms;
- ca += xms;
- alpha = atan2(sa,ca);
- delta = atan2(sd,sqrt(sa*sa+ca*ca));
-
- /*
- * here are the necessary elements of Saturn's rings
- * cf. Exp. Supp. p. 363ff.
- */
-
- capj = 6.9056 - 0.4322*capt;
- capn = 126.3615 + 3.9894*capt + 0.2403*capt2;
- eye = 28.0743 - 0.0128*capt;
- comg = 168.1179 + 1.3936*capt;
- omg = 42.9236 - 2.7390*capt - 0.2344*capt2;
-
- capj *= radian;
- capn *= radian;
- eye *= radian;
- comg *= radian;
- omg *= radian;
-
- /*
- * now find saturnicentric ring-plane coords of the earth
- */
-
- sb = sin(capj)*cos(delta)*sin(alpha-capn) -
- cos(capj)*sin(delta);
- su = cos(capj)*cos(delta)*sin(alpha-capn) +
- sin(capj)*sin(delta);
- cu = cos(delta)*cos(alpha-capn);
- u = atan2(su,cu);
- b = atan2(sb,sqrt(su*su+cu*cu));
-
- /*
- * and then the saturnicentric ring-plane coords of the sun
- */
-
- su = sin(eye)*sin(beta) +
- cos(eye)*cos(beta)*sin(lambda-comg);
- cu = cos(beta)*cos(lambda-comg);
- up = atan2(su,cu);
-
- /*
- * at last, the magnitude
- */
-
-
- sb = sin(b);
- mag = -8.68 +2.52*fabs(up+omg-u)-
- 2.60*fabs(sb) + 1.25*(sb*sb);
-
- helio();
- geo();
- }
-