| 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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