| 1 | #include <math.h>
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| 2 | 
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| 3 | #include <stdio.h>
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| 4 | 
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| 5 | #include "astro.h"
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| 6 | 
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| 7 | /* convert those orbital elements that change from epoch mj0 to epoch mj.
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| 8 |  */
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| 9 | void
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| 10 | reduce_elements (
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| 11 | double mj0,     /* initial epoch */
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| 12 | double mj,      /* desired epoch */
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| 13 | double inc0,    /* initial inclination, rads */
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| 14 | double ap0,     /* initial argument of perihelion, as an mj */
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| 15 | double om0,     /* initial long of ascending node, rads */
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| 16 | double *inc,    /* resultant inclination, rads */
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| 17 | double *ap,     /* resultant arg of perihelion, as an mj */
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| 18 | double *om)     /* resultant long of ascending node, rads */
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| 19 | {
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| 20 |         double t0, t1;
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| 21 |         double tt, tt2, t02, tt3;
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| 22 |         double eta, th, th0;
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| 23 |         double a, b;
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| 24 |         double dap;
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| 25 |         double cinc, sinc;
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| 26 |         double ot, sot, cot, ot1;
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| 27 |         double seta, ceta;
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| 28 | 
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| 29 |         if (fabs(mj - mj0) < 1e-5) {
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| 30 |             /* sin(eta) blows for inc < 10 degrees -- anyway, no need */
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| 31 |             *inc = inc0;
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| 32 |             *ap = ap0;
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| 33 |             *om = om0;
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| 34 |             return;
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| 35 |         }
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| 36 | 
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| 37 |         t0 = mj0/365250.0;
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| 38 |         t1 = mj/365250.0;
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| 39 | 
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| 40 |         tt = t1-t0;
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| 41 |         tt2 = tt*tt;
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| 42 |         t02 = t0*t0;
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| 43 |         tt3 = tt*tt2;
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| 44 |         eta = (471.07-6.75*t0+.57*t02)*tt+(.57*t0-3.37)*tt2+.05*tt3;
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| 45 |         th0 = 32869.0*t0+56*t02-(8694+55*t0)*tt+3*tt2;
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| 46 |         eta = degrad(eta/3600.0);
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| 47 |         th0 = degrad((th0/3600.0)+173.950833);
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| 48 |         th = (50256.41+222.29*t0+.26*t02)*tt+(111.15+.26*t0)*tt2+.1*tt3;
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| 49 |         th = th0+degrad(th/3600.0);
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| 50 |         cinc = cos(inc0);
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| 51 |         sinc = sin(inc0);
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| 52 |         ot = om0-th0;
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| 53 |         sot = sin(ot);
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| 54 |         cot = cos(ot);
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| 55 |         seta = sin(eta);
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| 56 |         ceta = cos(eta);
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| 57 |         a = sinc*sot;
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| 58 |         b = ceta*sinc*cot-seta*cinc;
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| 59 |         ot1 = atan(a/b);
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| 60 |         if (b<0) ot1 += PI;
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| 61 |         b = sinc*ceta-cinc*seta*cot;
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| 62 |         a = -1*seta*sot;
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| 63 |         dap = atan(a/b);
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| 64 |         if (b<0) dap += PI;
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| 65 | 
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| 66 |         *ap = ap0+dap;
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| 67 |         range (ap, 2*PI);
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| 68 |         *om = ot1+th;
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| 69 |         range (om, 2*PI);
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| 70 | 
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| 71 |         if (inc0<.175)
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| 72 |             *inc = asin(a/sin(dap));
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| 73 |         else
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| 74 |             *inc = 1.570796327-asin((cinc*ceta)+(sinc*seta*cot));
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| 75 | }
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| 76 | 
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| 77 | /* For RCS Only -- Do Not Edit */
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| 78 | static char *rcsid[2] = {(char *)rcsid, "@(#) $RCSfile: reduce.c,v $ $Date: 2006-11-22 13:53:30 $ $Revision: 1.6 $ $Name: not supported by cvs2svn $"};
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