| 1 | /* heliocentric rectangular equatorial coordinates of Jupiter to Pluto; | 
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| 2 | * from Chapront's expansion of DE200/extension of DE200;  mean equator J2000.0 | 
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| 3 | * | 
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| 4 | * calculation time (milliseconds) on an HP 715/75, Jupiter to Pluto: | 
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| 5 | * (each coordinate component counted as 1 term, | 
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| 6 | * secular terms included for JD 2448908.5 = 1992 Oct 13.0) | 
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| 7 | * | 
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| 8 | *      prec    terms   rates   no rates | 
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| 9 | *      0.0     2256    5.1     4.6 | 
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| 10 | * | 
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| 11 | *      1e-7    792     2.6     2.4     --> nominal precision rel. to DE200 | 
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| 12 | *      1e-6    535     2.1     2.0 | 
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| 13 | *      1e-5    350     1.8     1.6 | 
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| 14 | *      1e-4    199     1.5     1.4 | 
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| 15 | *      1e-3    96      1.2     1.1 | 
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| 16 | * | 
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| 17 | *      no drop 2256    4.5     3.9     (code without test criterion) | 
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| 18 | */ | 
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| 19 |  | 
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| 20 | #include <math.h> | 
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| 21 |  | 
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| 22 | #include "astro.h" | 
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| 23 | #include "chap95.h" | 
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| 24 |  | 
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| 25 | #define CHAP_MAXTPOW    2       /* NB: valid for all 5 outer planets */ | 
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| 26 |  | 
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| 27 | /* chap95() | 
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| 28 | * | 
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| 29 | * input: | 
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| 30 | *      m       modified JD; days from J1900.0 = 2415020.0 | 
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| 31 | * | 
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| 32 | *      prec    precision level, in radians. | 
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| 33 | *              if (prec = 0.0), you get the full precision, namely | 
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| 34 | *              a deviation of not more than 0.02 arc seconds (1e-7 rad) | 
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| 35 | *              from the JPL DE200 integration, on which this expansion | 
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| 36 | *              is based. | 
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| 37 | * | 
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| 38 | *      obj     object number as in astro.h (jupiter=3, saturn=4, ...) | 
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| 39 | * | 
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| 40 | * output: | 
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| 41 | *      ret[6]  cartesian components of position and velocity | 
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| 42 | * | 
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| 43 | * return: | 
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| 44 | *      0       Ok | 
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| 45 | *      1       time out of range [CHAP_BEGIN .. CHAP_END] | 
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| 46 | *      2       object out of range [JUPITER .. PLUTO] | 
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| 47 | *      3       precision out of range [0.0 .. 1e-3] | 
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| 48 | */ | 
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| 49 | int | 
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| 50 | chap95 (double m, int obj, double prec, double *ret) | 
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| 51 | { | 
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| 52 | static double a0[] = {          /* semimajor axes for precision ctrl */ | 
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| 53 | 0.39, 0.72, 1.5, 5.2, 9.6, 19.2, 30.1, 39.5, 1.0 | 
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| 54 | }; | 
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| 55 | double sum[CHAP_MAXTPOW+1][6];  /* [T^0, ..][X,Y,Z,X',Y',Z'] */ | 
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| 56 | double T, t;                    /* time in centuries and years */ | 
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| 57 | double ca, sa, Nu;              /* aux vars for terms */ | 
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| 58 | double precT[CHAP_MAXTPOW+1];   /* T-augmented precision threshold */ | 
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| 59 | chap95_rec *rec;                /* term coeffs */ | 
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| 60 | int cooidx; | 
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| 61 |  | 
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| 62 | /* check parameters */ | 
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| 63 | if (m < CHAP_BEGIN || m > CHAP_END) | 
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| 64 | return (1); | 
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| 65 |  | 
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| 66 | if (obj < JUPITER || obj > PLUTO) | 
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| 67 | return (2); | 
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| 68 |  | 
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| 69 | if (prec < 0.0 || prec > 1e-3) | 
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| 70 | return (3); | 
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| 71 |  | 
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| 72 | /* init the sums */ | 
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| 73 | zero_mem ((void *)sum, sizeof(sum)); | 
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| 74 |  | 
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| 75 | T = (m - J2000)/36525.0;        /* centuries since J2000.0 */ | 
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| 76 |  | 
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| 77 | /* modify precision treshold for | 
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| 78 | * a) term storing scale | 
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| 79 | * b) convert radians to au | 
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| 80 | * c) account for skipped terms (more terms needed for better prec) | 
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| 81 | *    threshold empirically established similar to VSOP; stern | 
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| 82 | * d) augment for secular terms | 
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| 83 | */ | 
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| 84 | precT[0] = prec * CHAP_SCALE                            /* a) */ | 
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| 85 | * a0[obj]                               /* b) */ | 
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| 86 | / (10. * (-log10(prec + 1e-35) - 2));   /* c) */ | 
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| 87 | t = 1./(fabs(T) + 1e-35);                               /* d) */ | 
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| 88 | precT[1] = precT[0]*t; | 
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| 89 | precT[2] = precT[1]*t; | 
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| 90 |  | 
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| 91 | t = T * 100.0;          /* YEARS since J2000.0 */ | 
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| 92 |  | 
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| 93 | ca = sa = Nu = 0.;      /* shut up compiler warning 'uninitialised' */ | 
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| 94 |  | 
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| 95 | switch (obj) {          /* set initial term record pointer */ | 
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| 96 | case JUPITER:       rec = chap95_jupiter;   break; | 
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| 97 | case SATURN:        rec = chap95_saturn;    break; | 
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| 98 | case URANUS:        rec = chap95_uranus;    break; | 
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| 99 | case NEPTUNE:       rec = chap95_neptune;   break; | 
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| 100 | case PLUTO:         rec = chap95_pluto;     break; | 
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| 101 | default: | 
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| 102 | return (2);     /* wrong object: severe internal trouble */ | 
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| 103 | } | 
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| 104 |  | 
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| 105 | /* do the term summation into sum[T^n] slots */ | 
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| 106 | for (; rec->n >= 0; ++rec) { | 
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| 107 | double *amp; | 
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| 108 |  | 
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| 109 | /* NOTE:  The formula | 
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| 110 | * X = SUM[i=1,Records] T**n_i*(CX_i*cos(Nu_k*t)+SX_i*sin(Nu_k*t)) | 
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| 111 | * could be rewritten as  SUM( ... A sin (B + C*t) ) | 
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| 112 | * "saving" trigonometric calls.  However, e.g. for Pluto, | 
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| 113 | * there are only 65 distinct angles NU_k (130 trig calls). | 
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| 114 | * With that manipulation, EVERY arg_i would be different for X, | 
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| 115 | * Y and Z, which is 3*96 terms.  Hence, the formulation as | 
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| 116 | * given is good (optimal?). | 
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| 117 | */ | 
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| 118 |  | 
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| 119 | for (cooidx = 0, amp = rec->amp; cooidx < 3; ++cooidx) { | 
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| 120 | double C, S, term, termdot; | 
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| 121 | short n;                /* fast access */ | 
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| 122 |  | 
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| 123 | C = *amp++; | 
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| 124 | S = *amp++; | 
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| 125 | n = rec->n; | 
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| 126 |  | 
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| 127 | /* drop term if too small | 
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| 128 | * this is quite expensive:  17% of loop time | 
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| 129 | */ | 
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| 130 | if (fabs(C) + fabs(S) < precT[n]) | 
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| 131 | continue; | 
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| 132 |  | 
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| 133 | if (n == 0 && cooidx == 0) {    /* new Nu only here */ | 
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| 134 | double arg; | 
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| 135 |  | 
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| 136 | Nu = rec->Nu; | 
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| 137 | arg = Nu * t; | 
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| 138 | arg -= floor(arg/(2.*PI))*(2.*PI); | 
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| 139 | ca = cos(arg);      /* blast it - even for Nu = 0.0 */ | 
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| 140 | sa = sin(arg); | 
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| 141 | } | 
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| 142 |  | 
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| 143 | term = C * ca + S * sa; | 
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| 144 | sum[n][cooidx] += term; | 
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| 145 | #if CHAP_GETRATE | 
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| 146 | termdot = (-C * sa + S * ca) * Nu; | 
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| 147 | sum[n][cooidx+3] += termdot; | 
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| 148 | if (n > 0) sum[n - 1][cooidx+3] += n/100.0 * term; | 
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| 149 | #endif | 
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| 150 | } /* cooidx */ | 
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| 151 | } /* records */ | 
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| 152 |  | 
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| 153 | /* apply powers of time and sum up */ | 
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| 154 | for (cooidx = 0; cooidx < 6; ++cooidx) { | 
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| 155 | ret[cooidx] = (sum[0][cooidx] + | 
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| 156 | T * (sum[1][cooidx] + | 
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| 157 | T * (sum[2][cooidx] )) )/CHAP_SCALE; | 
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| 158 | } | 
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| 159 |  | 
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| 160 | /* TEST: if the MAIN terms are dropped, get angular residue | 
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| 161 | ret[0] = sqrt(ret[0]*ret[0] + ret[1]*ret[1] + ret[2]*ret[2])/a0[obj]; | 
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| 162 | */ | 
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| 163 |  | 
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| 164 | #if CHAP_GETRATE | 
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| 165 | for (cooidx = 3; cooidx < 6; ++cooidx) { | 
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| 166 | ret[cooidx] /= 365.25;      /* yearly to daily rate */ | 
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| 167 | } | 
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| 168 | #endif | 
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| 169 |  | 
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| 170 | return (0); | 
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| 171 | } | 
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| 172 |  | 
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| 173 | /* For RCS Only -- Do Not Edit */ | 
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| 174 | static char *rcsid[2] = {(char *)rcsid, "@(#) $RCSfile: chap95.c,v $ $Date: 2005-08-21 10:02:36 $ $Revision: 1.5 $ $Name: not supported by cvs2svn $"}; | 
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