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[dockapps.git] / wmweather+ / sunzenith.c
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1 #include "config.h"
3 /* Copyright (C) 2002 Brad Jorsch <anomie@users.sourceforge.net>
5 This program is free software; you can redistribute it and/or modify
6 it under the terms of the GNU General Public License as published by
7 the Free Software Foundation; either version 2 of the License, or
8 (at your option) any later version.
10 This program is distributed in the hope that it will be useful,
11 but WITHOUT ANY WARRANTY; without even the implied warranty of
12 MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
13 GNU General Public License for more details.
15 You should have received a copy of the GNU General Public License
16 along with this program; if not, write to the Free Software
17 Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301 USA
20 /* Algorithms from http://www.srrb.noaa.gov/highlights/sunrise/azel.html */
22 #include <stdio.h>
23 #include <math.h>
24 #include <time.h>
25 #include <stdlib.h>
26 #include <limits.h>
28 #include "convert.h"
30 /* Purpose: calculate the Geometric Mean Longitude of the Sun (degrees) */
31 double calcGeomMeanLongSun(double t) {
32 double L0 = 280.46646 + t * (36000.76983 + 0.0003032 * t);
33 while(L0 > 360.0) {
34 L0 -= 360.0;
36 while(L0 < 0.0) {
37 L0 += 360.0;
39 return L0;
43 /* Purpose: calculate the Geometric Mean Anomaly of the Sun (degrees) */
44 double calcGeomMeanAnomalySun(double t) {
45 return 357.52911 + t * (35999.05029 - 0.0001537 * t);
49 /* Purpose: calculate the eccentricity of earth's orbit */
50 double calcEccentricityEarthOrbit(double t) {
51 return 0.016708634 - t * (0.000042037 + 0.0000001267 * t);
55 /* Purpose: calculate the equation of center for the sun (degrees) */
56 double calcSunEqOfCenter(double t) {
57 double m = deg2rad(calcGeomMeanAnomalySun(t));
59 return sin(m) * (1.914602 - t * (0.004817 + 0.000014 * t)) + sin(m+m) * (0.019993 - 0.000101 * t) + sin(m+m+m) * 0.000289;
63 /* Purpose: calculate the true longitude of the sun (degrees) */
64 double calcSunTrueLong(double t) {
65 return calcGeomMeanLongSun(t) + calcSunEqOfCenter(t);
69 /* Purpose: calculate the apparent longitude of the sun (degrees) */
70 double calcSunApparentLong(double t) {
71 return calcSunTrueLong(t) - 0.00569 - 0.00478 * sin(deg2rad(125.04-1934.136*t));
75 /* Purpose: calculate the mean obliquity of the ecliptic (degrees) */
76 double calcMeanObliquityOfEcliptic(double t) {
77 return 23.0 + (26.0 + ((21.448 - t*(46.8150 + t*(0.00059 - t*(0.001813))))/60.0))/60.0;
81 /* Purpose: calculate the corrected obliquity of the ecliptic (degrees) */
82 double calcObliquityCorrection(double t) {
83 return calcMeanObliquityOfEcliptic(t) + 0.00256*cos(deg2rad(125.04-1934.136*t));
87 /* Purpose: calculate the declination of the sun (degrees) */
88 double calcSunDeclination(double t) {
89 return rad2deg(asin(sin(deg2rad(calcObliquityCorrection(t))) *
90 sin(deg2rad(calcSunApparentLong(t)))));
94 /* Purpose: calculate the difference between true solar time and mean
95 * solar time (minutes)
97 double calcEquationOfTime(double t) {
98 double l0 = deg2rad(calcGeomMeanLongSun(t));
99 double e = calcEccentricityEarthOrbit(t);
100 double m = deg2rad(calcGeomMeanAnomalySun(t));
101 double y = tan(deg2rad(calcObliquityCorrection(t))/2.0);
102 double sinm = sin(m);
104 y *= y;
106 return rad2deg(y*sin(2.0*l0) - 2.0*e*sinm + 4.0*e*y*sinm*cos(2.0*l0)
107 - 0.5*y*y*sin(4.0*l0) - 1.25*e*e*sin(2.0*m))*4.0;
111 double calcSolarZenith(double latitude, double longitude, int year, int month, int day, int timeUTC){
112 double T, trueSolarTime, hourAngle, solarDec, csz, zenith, exoatmElevation, te, refractionCorrection;
114 T=jd2jcent(mdy2jd(year, month, day) + timeUTC/1440.0);
115 trueSolarTime = timeUTC + calcEquationOfTime(T) - 4.0 * longitude;
116 hourAngle = trueSolarTime / 4.0 - 180.0;
117 solarDec = calcSunDeclination(T);
118 csz = sin(deg2rad(latitude)) * sin(deg2rad(solarDec)) +
119 cos(deg2rad(latitude)) * cos(deg2rad(solarDec)) *
120 cos(deg2rad(hourAngle));
121 zenith=rad2deg(acos(csz));
122 exoatmElevation = 90.0 - zenith;
123 if (exoatmElevation > 85.0) {
124 refractionCorrection = 0.0;
125 } else {
126 te = tan(deg2rad(exoatmElevation));
127 if (exoatmElevation > 5.0) {
128 refractionCorrection = 58.1/te - 0.07/(te*te*te) +
129 0.000086/(te*te*te*te*te);
130 } else if (exoatmElevation > -0.575) {
131 refractionCorrection = 1735.0 + exoatmElevation*(-518.2 + exoatmElevation*(103.4 + exoatmElevation*(-12.79 + exoatmElevation*0.711)));
132 } else {
133 refractionCorrection = -20.774 / te;
135 refractionCorrection = refractionCorrection / 3600.0;
137 return zenith - refractionCorrection;