Astro with some minor changes to placate Unix.
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126
src/cmd/astro/venus.c
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126
src/cmd/astro/venus.c
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#include "astro.h"
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void
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venus(void)
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{
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double pturbl, pturbb, pturbr;
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double lograd;
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double dele, enom, vnom, nd, sl;
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double v0, t0, m0, j0, s0;
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double lsun, elong, ci, dlong;
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/*
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* here are the mean orbital elements
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*/
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ecc = .00682069 - .00004774*capt + 0.091e-6*capt2;
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incl = 3.393631 + .0010058*capt - 0.97e-6*capt2;
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node = 75.779647 + .89985*capt + .00041*capt2;
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argp = 130.163833 + 1.408036*capt - .0009763*capt2;
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mrad = .7233316;
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anom = 212.603219 + 1.6021301540*eday + .00128605*capt2;
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motion = 1.6021687039;
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/*
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* mean anomalies of perturbing planets
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*/
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v0 = 212.60 + 1.602130154*eday;
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t0 = 358.63 + .985608747*eday;
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m0 = 319.74 + 0.524032490*eday;
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j0 = 225.43 + .083090842*eday;
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s0 = 175.8 + .033459258*eday;
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v0 *= radian;
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t0 *= radian;
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m0 *= radian;
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j0 *= radian;
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s0 *= radian;
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incl *= radian;
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node *= radian;
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argp *= radian;
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anom = fmod(anom, 360.)*radian;
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/*
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* computation of long period terms affecting the mean anomaly
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*/
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anom +=
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(2.761-0.022*capt)*radsec*sin(
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13.*t0 - 8.*v0 + 43.83*radian + 4.52*radian*capt)
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+ 0.268*radsec*cos(4.*m0 - 7.*t0 + 3.*v0)
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+ 0.019*radsec*sin(4.*m0 - 7.*t0 + 3.*v0)
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- 0.208*radsec*sin(s0 + 1.4*radian*capt);
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/*
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* computation of elliptic orbit
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*/
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enom = anom + ecc*sin(anom);
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do {
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dele = (anom - enom + ecc * sin(enom)) /
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(1 - ecc*cos(enom));
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enom += dele;
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} while(fabs(dele) > converge);
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vnom = 2*atan2(sqrt((1+ecc)/(1-ecc))*sin(enom/2),
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cos(enom/2));
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rad = mrad*(1 - ecc*cos(enom));
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lambda = vnom + argp;
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/*
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* perturbations in longitude
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*/
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icosadd(venfp, vencp);
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pturbl = cosadd(4, v0, t0, m0, j0);
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pturbl *= radsec;
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/*
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* perturbations in latidude
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*/
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pturbb = cosadd(3, v0, t0, j0);
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pturbb *= radsec;
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/*
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* perturbations in log radius vector
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*/
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pturbr = cosadd(4, v0, t0, m0, j0);
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/*
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* reduction to the ecliptic
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*/
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lambda += pturbl;
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nd = lambda - node;
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lambda = node + atan2(sin(nd)*cos(incl),cos(nd));
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sl = sin(incl)*sin(nd);
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beta = atan2(sl, pyth(sl)) + pturbb;
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lograd = pturbr*2.30258509;
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rad *= 1 + lograd;
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motion *= radian*mrad*mrad/(rad*rad);
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/*
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* computation of magnitude
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*/
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lsun = 99.696678 + 0.9856473354*eday;
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lsun *= radian;
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elong = lambda - lsun;
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ci = (rad - cos(elong))/sqrt(1 + rad*rad - 2*rad*cos(elong));
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dlong = atan2(pyth(ci), ci)/radian;
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mag = -4 + .01322*dlong + .0000004247*dlong*dlong*dlong;
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semi = 8.41;
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helio();
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geo();
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}
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