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Phase.c
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Phase.c
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/*
* Phase.c
*
* Created by Craig Hockenberry on Mon Jul 21 2003.
*/
#include "Phase.h"
#include "MathDefinitions.h"
/* Adapted from "moontool.c" by John Walker, Release 2.0. */
#include <stdio.h>
#include <math.h>
//#include "tws.h"
/* Astronomical constants. */
#define epoch 2444238.5 /* 1980 January 0.0 */
/* Constants defining the Sun's apparent orbit. */
#define elonge 278.833540 /* ecliptic longitude of the Sun
at epoch 1980.0 */
#define elongp 282.596403 /* ecliptic longitude of the Sun at
perigee */
#define eccent 0.016718 /* eccentricity of Earth's orbit */
#define sunsmax 1.495985e8 /* semi-major axis of Earth's orbit, km */
#define sunangsiz 0.533128 /* sun's angular size, degrees, at
semi-major axis distance */
/* Elements of the Moon's orbit, epoch 1980.0. */
#define mmlong 64.975464 /* moon's mean lonigitude at the epoch */
#define mmlongp 349.383063 /* mean longitude of the perigee at the
epoch */
#define mlnode 151.950429 /* mean longitude of the node at the
epoch */
#define minc 5.145396 /* inclination of the Moon's orbit */
#define mecc 0.054900 /* eccentricity of the Moon's orbit */
#define mangsiz 0.5181 /* moon's angular size at distance a
from Earth */
#define msmax 384401.0 /* semi-major axis of Moon's orbit in km */
#define mparallax 0.9507 /* parallax at distance a from Earth */
#define lunatbase 2423436.0 /* base date for E. W. Brown's numbered
series of lunations (1923 January 16) */
/* Properties of the Earth. */
#define earthrad 6378.16 /* radius of Earth in kilometres */
/* jdate - convert internal GMT date and time to Julian day and fraction */
static long jdate(struct tm* t)
//struct tws *t;
{
long c, m, y;
y = t->tm_year + 1900;
m = t->tm_mon + 1;
if (m > 2)
m = m - 3;
else {
m = m + 9;
--y;
}
c = y / 100L; /* compute century */
y -= 100L * c;
return (t->tm_mday + (c * 146097L) / 4 + (y * 1461L) / 4 + (m * 153L + 2) / 5 + 1721119L);
}
/* jtime - convert internal date and time to astronomical Julian
** time (i.e. Julian date plus day fraction, expressed as
** a double)
*/
double jtime(struct tm* t)
//struct tws *t;
{
// int c;
//
// c = - t->tw_zone;
// if ( t->tw_flags & TW_DST )
// c += 60;
// return (jdate(t) - 0.5) + (t->tw_sec + 60 * (t->tw_min + c + 60 * t->tw_hour)) / 86400.0;
return (((double)jdate(t) - 0.5) + (double)(t->tm_sec + 60 * (t->tm_min + 60 * t->tm_hour)) / 86400.0);
}
/* jyear - convert Julian date to year, month, day, which are
** returned via integer pointers to integers
*/
static void jyear(td, yy, mm, dd)
double td;
int *yy, *mm, *dd;
{
double j, d, y, m;
td += 0.5; /* astronomical to civil */
j = floor(td);
j = j - 1721119.0;
y = floor(((4 * j) - 1) / 146097.0);
j = (j * 4.0) - (1.0 + (146097.0 * y));
d = floor(j / 4.0);
j = floor(((4.0 * d) + 3.0) / 1461.0);
d = ((4.0 * d) + 3.0) - (1461.0 * j);
d = floor((d + 4.0) / 4.0);
m = floor(((5.0 * d) - 3) / 153.0);
d = (5.0 * d) - (3.0 + (153.0 * m));
d = floor((d + 5.0) / 5.0);
y = (100.0 * y) + j;
if (m < 10.0)
m = m + 3;
else {
m = m - 9;
y = y + 1;
}
*yy = y;
*mm = m;
*dd = d;
}
/* meanphase - calculates mean phase of the Moon for a given base date
** and desired phase:
** 0.0 New Moon
** 0.25 First quarter
** 0.5 Full moon
** 0.75 Last quarter
** Beware!!! This routine returns meaningless
** results for any other phase arguments. Don't
** attempt to generalise it without understanding
** that the motion of the moon is far more complicated
** that this calculation reveals.
*/
static double meanphase(sdate, phase, usek)
double sdate, phase;
double *usek;
{
int yy, mm, dd;
double k, t, t2, t3, nt1;
jyear(sdate, &yy, &mm, &dd);
k = (yy + ((mm - 1) * (1.0 / 12.0)) - 1900) * 12.3685;
/* Time in Julian centuries from 1900 January 0.5. */
t = (sdate - 2415020.0) / 36525;
t2 = t * t; /* square for frequent use */
t3 = t2 * t; /* cube for frequent use */
*usek = k = floor(k) + phase;
nt1 = 2415020.75933 + synmonth * k
+ 0.0001178 * t2
- 0.000000155 * t3
+ 0.00033 * dsin(166.56 + 132.87 * t - 0.009173 * t2);
return nt1;
}
/* truephase - given a K value used to determine the mean phase of the
** new moon, and a phase selector (0.0, 0.25, 0.5, 0.75),
** obtain the true, corrected phase time
*/
static double truephase(k, phase)
double k, phase;
{
double t, t2, t3, pt, m, mprime, f;
int apcor = 0;
k += phase; /* add phase to new moon time */
t = k / 1236.85; /* time in Julian centuries from
1900 January 0.5 */
t2 = t * t; /* square for frequent use */
t3 = t2 * t; /* cube for frequent use */
pt = 2415020.75933 /* mean time of phase */
+ synmonth * k
+ 0.0001178 * t2
- 0.000000155 * t3
+ 0.00033 * dsin(166.56 + 132.87 * t - 0.009173 * t2);
m = 359.2242 /* Sun's mean anomaly */
+ 29.10535608 * k
- 0.0000333 * t2
- 0.00000347 * t3;
mprime = 306.0253 /* Moon's mean anomaly */
+ 385.81691806 * k
+ 0.0107306 * t2
+ 0.00001236 * t3;
f = 21.2964 /* Moon's argument of latitude */
+ 390.67050646 * k
- 0.0016528 * t2
- 0.00000239 * t3;
if ((phase < 0.01) || (abs(phase - 0.5) < 0.01)) {
/* Corrections for New and Full Moon. */
pt += (0.1734 - 0.000393 * t) * dsin(m)
+ 0.0021 * dsin(2 * m)
- 0.4068 * dsin(mprime)
+ 0.0161 * dsin(2 * mprime)
- 0.0004 * dsin(3 * mprime)
+ 0.0104 * dsin(2 * f)
- 0.0051 * dsin(m + mprime)
- 0.0074 * dsin(m - mprime)
+ 0.0004 * dsin(2 * f + m)
- 0.0004 * dsin(2 * f - m)
- 0.0006 * dsin(2 * f + mprime)
+ 0.0010 * dsin(2 * f - mprime)
+ 0.0005 * dsin(m + 2 * mprime);
apcor = 1;
} else if ((abs(phase - 0.25) < 0.01 || (abs(phase - 0.75) < 0.01))) {
pt += (0.1721 - 0.0004 * t) * dsin(m)
+ 0.0021 * dsin(2 * m)
- 0.6280 * dsin(mprime)
+ 0.0089 * dsin(2 * mprime)
- 0.0004 * dsin(3 * mprime)
+ 0.0079 * dsin(2 * f)
- 0.0119 * dsin(m + mprime)
- 0.0047 * dsin(m - mprime)
+ 0.0003 * dsin(2 * f + m)
- 0.0004 * dsin(2 * f - m)
- 0.0006 * dsin(2 * f + mprime)
+ 0.0021 * dsin(2 * f - mprime)
+ 0.0003 * dsin(m + 2 * mprime)
+ 0.0004 * dsin(m - 2 * mprime)
- 0.0003 * dsin(2 * m + mprime);
if (phase < 0.5)
/* First quarter correction. */
pt += 0.0028 - 0.0004 * dcos(m) + 0.0003 * dcos(mprime);
else
/* Last quarter correction. */
pt += -0.0028 + 0.0004 * dcos(m) - 0.0003 * dcos(mprime);
apcor = 1;
}
if (!apcor) {
(void) fprintf(stderr, "truephase() called with invalid phase selector.\n");
pt = 0.0;
}
return pt;
}
/* phasehunt5 - find time of phases of the moon which surround the current
** date. Five phases are found, starting and ending with the
** new moons which bound the current lunation
*/
void phasehunt5(sdate, phases)
double sdate;
double phases[5];
{
double adate, k1, k2, nt1, nt2;
adate = sdate - 45;
nt1 = meanphase(adate, 0.0, &k1);
for ( ; ; ) {
adate += synmonth;
nt2 = meanphase(adate, 0.0, &k2);
if (nt1 <= sdate && nt2 > sdate)
break;
nt1 = nt2;
k1 = k2;
}
phases[0] = truephase(k1, 0.0);
phases[1] = truephase(k1, 0.25);
phases[2] = truephase(k1, 0.5);
phases[3] = truephase(k1, 0.75);
phases[4] = truephase(k2, 0.0);
}
/* phasehunt2 - find time of phases of the moon which surround the current
** date. Two phases are found.
*/
void phasehunt2(sdate, phases, which)
double sdate;
double phases[2];
double which[2];
{
double adate, k1, k2, nt1, nt2;
adate = sdate - 45;
nt1 = meanphase(adate, 0.0, &k1);
for ( ; ; ) {
adate += synmonth;
nt2 = meanphase(adate, 0.0, &k2);
if (nt1 <= sdate && nt2 > sdate)
break;
nt1 = nt2;
k1 = k2;
}
phases[0] = truephase(k1, 0.0);
which[0] = 0.0;
phases[1] = truephase(k1, 0.25);
which[1] = 0.25;
if ( phases[1] <= sdate ) {
phases[0] = phases[1];
which[0] = which[1];
phases[1] = truephase(k1, 0.5);
which[1] = 0.5;
if ( phases[1] <= sdate ) {
phases[0] = phases[1];
which[0] = which[1];
phases[1] = truephase(k1, 0.75);
which[1] = 0.75;
if ( phases[1] <= sdate ) {
phases[0] = phases[1];
which[0] = which[1];
phases[1] = truephase(k2, 0.0);
which[1] = 0.0;
}
}
}
}
/* kepler - solve the equation of Kepler */
static double kepler(m, ecc)
double m, ecc;
{
double e, delta;
#define EPSILON 1E-6
e = m = torad(m);
do {
delta = e - ecc * sin(e) - m;
e -= delta / (1 - ecc * cos(e));
} while (abs(delta) > EPSILON);
return e;
}
/* phase - calculate phase of moon as a fraction:
**
** The argument is the time for which the phase is requested,
** expressed as a Julian date and fraction. Returns the terminator
** phase angle as a percentage of a full circle (i.e., 0 to 1),
** and stores into pointer arguments the illuminated fraction of
** the Moon's disc, the Moon's age in days and fraction, the
** distance of the Moon from the centre of the Earth, and the
** angular diameter subtended by the Moon as seen by an observer
** at the centre of the Earth.
*/
//double pdate;
//double *pphase; /* illuminated fraction */
//double *mage; /* age of moon in days */
//double *dist; /* distance in kilometres */
//double *angdia; /* angular diameter in degrees */
//double *sudist; /* distance to Sun */
//double *suangdia; /* sun's angular diameter */
double phase(double pdate, double *pphase, double *mage, double *dist, double *angdia, double *sudist, double *suangdia)
{
double Day, N, M, Ec, Lambdasun, ml, MM, Ev, Ae, A3, MmP,
mEc, A4, lP, V, lPP,
MoonAge, MoonPhase,
MoonDist, MoonDFrac, MoonAng,
F, SunDist, SunAng;
/* Calculation of the Sun's position. */
Day = pdate - epoch; /* date within epoch */
N = fixangle((360 / 365.2422) * Day); /* mean anomaly of the Sun */
M = fixangle(N + elonge - elongp); /* convert from perigee
co-ordinates to epoch 1980.0 */
Ec = kepler(M, eccent); /* solve equation of Kepler */
Ec = sqrt((1 + eccent) / (1 - eccent)) * tan(Ec / 2);
Ec = 2 * todeg(atan(Ec)); /* true anomaly */
Lambdasun = fixangle(Ec + elongp); /* Sun's geocentric ecliptic
longitude */
/* Orbital distance factor. */
F = ((1 + eccent * cos(torad(Ec))) / (1 - eccent * eccent));
SunDist = sunsmax / F; /* distance to Sun in km */
SunAng = F * sunangsiz; /* Sun's angular size in degrees */
/* Calculation of the Moon's position. */
/* Moon's mean longitude. */
ml = fixangle(13.1763966 * Day + mmlong);
/* Moon's mean anomaly. */
MM = fixangle(ml - 0.1114041 * Day - mmlongp);
/* Evection. */
Ev = 1.2739 * sin(torad(2 * (ml - Lambdasun) - MM));
/* Annual equation. */
Ae = 0.1858 * sin(torad(M));
/* Correction term. */
A3 = 0.37 * sin(torad(M));
/* Corrected anomaly. */
MmP = MM + Ev - Ae - A3;
/* Correction for the equation of the centre. */
mEc = 6.2886 * sin(torad(MmP));
/* Another correction term. */
A4 = 0.214 * sin(torad(2 * MmP));
/* Corrected longitude. */
lP = ml + Ev + mEc - Ae + A4;
/* Variation. */
V = 0.6583 * sin(torad(2 * (lP - Lambdasun)));
/* True longitude. */
lPP = lP + V;
/* Calculation of the phase of the Moon. */
/* Age of the Moon in degrees. */
MoonAge = lPP - Lambdasun;
/* Phase of the Moon. */
MoonPhase = (1 - cos(torad(MoonAge))) / 2;
/* Calculate distance of moon from the centre of the Earth. */
MoonDist = (msmax * (1 - mecc * mecc)) /
(1 + mecc * cos(torad(MmP + mEc)));
/* Calculate Moon's angular diameter. */
MoonDFrac = MoonDist / msmax;
MoonAng = mangsiz / MoonDFrac;
*pphase = MoonPhase;
*mage = synmonth * (fixangle(MoonAge) / 360.0);
*dist = MoonDist;
*angdia = MoonAng;
*sudist = SunDist;
*suangdia = SunAng;
return torad(fixangle(MoonAge));
}