1 /**************************************************************************
3 * Written by Durk Talsma. Originally started October 1997, for distribution
4 * with the FlightGear project. Version 2 was written in August and
5 * September 1998. This code is based upon algorithms and data kindly
6 * provided by Mr. Paul Schlyter. (pausch@saaf.se).
8 * This library is free software; you can redistribute it and/or
9 * modify it under the terms of the GNU Library General Public
10 * License as published by the Free Software Foundation; either
11 * version 2 of the License, or (at your option) any later version.
13 * This library is distributed in the hope that it will be useful,
14 * but WITHOUT ANY WARRANTY; without even the implied warranty of
15 * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
16 * Library General Public License for more details.
18 * You should have received a copy of the GNU Library General Public
19 * License along with this library; if not, write to the
20 * Free Software Foundation, Inc., 59 Temple Place - Suite 330,
21 * Boston, MA 02111-1307, USA.
24 **************************************************************************/
29 #include <simgear/debug/logstream.hxx>
30 #include <simgear/misc/fgpath.hxx>
33 # define exception c_exception
37 // #include <FDM/flight.hxx>
42 /*************************************************************************
43 * Moon::Moon(double mjd)
44 * Public constructor for class Moon. Initializes the orbital elements and
45 * sets up the moon texture.
46 * Argument: The current time.
47 * the hard coded orbital elements for Moon are passed to
48 * CelestialBody::CelestialBody();
49 ************************************************************************/
50 Moon::Moon(double mjd) :
51 CelestialBody(125.1228, -0.0529538083,
53 318.0634, 0.1643573223,
56 115.3654, 13.0649929509, mjd)
61 CelestialBody(125.1228, -0.0529538083,
63 318.0634, 0.1643573223,
66 115.3654, 13.0649929509)
76 /*****************************************************************************
77 * void Moon::updatePosition(double mjd, Star *ourSun)
78 * this member function calculates the actual topocentric position (i.e.)
79 * the position of the moon as seen from the current position on the surface
81 ****************************************************************************/
82 void Moon::updatePosition(double mjd, double lst, double lat, Star *ourSun)
85 eccAnom, ecl, actTime,
86 xv, yv, v, r, xh, yh, zh, xg, yg, zg, xe, ye, ze,
87 Ls, Lm, D, F, mpar, gclat, rho, HA, g,
90 updateOrbElements(mjd);
91 actTime = sgCalcActTime(mjd);
93 // calculate the angle between ecliptic and equatorial coordinate system
95 ecl = ((DEG_TO_RAD * 23.4393) - (DEG_TO_RAD * 3.563E-7) * actTime);
96 eccAnom = sgCalcEccAnom(M, e); // Calculate the eccentric anomaly
97 xv = a * (cos(eccAnom) - e);
98 yv = a * (sqrt(1.0 - e*e) * sin(eccAnom));
99 v = atan2(yv, xv); // the moon's true anomaly
100 r = sqrt (xv*xv + yv*yv); // and its distance
102 // estimate the geocentric rectangular coordinates here
103 xh = r * (cos(N) * cos (v+w) - sin (N) * sin(v+w) * cos(i));
104 yh = r * (sin(N) * cos (v+w) + cos (N) * sin(v+w) * cos(i));
105 zh = r * (sin(v+w) * sin(i));
107 // calculate the ecliptic latitude and longitude here
108 lonEcl = atan2 (yh, xh);
109 latEcl = atan2(zh, sqrt(xh*xh + yh*yh));
111 /* Calculate a number of perturbatioin, i.e. disturbances caused by the
112 * gravitational infuence of the sun and the other major planets.
113 * The largest of these even have a name */
114 Ls = ourSun->getM() + ourSun->getw();
119 lonEcl += DEG_TO_RAD * (-1.274 * sin (M - 2*D)
121 -0.186 * sin(ourSun->getM())
122 -0.059 * sin(2*M - 2*D)
123 -0.057 * sin(M - 2*D + ourSun->getM())
124 +0.053 * sin(M + 2*D)
125 +0.046 * sin(2*D - ourSun->getM())
126 +0.041 * sin(M - ourSun->getM())
128 -0.031 * sin(M + ourSun->getM())
129 -0.015 * sin(2*F - 2*D)
130 +0.011 * sin(M - 4*D)
132 latEcl += DEG_TO_RAD * (-0.173 * sin(F-2*D)
133 -0.055 * sin(M - F - 2*D)
134 -0.046 * sin(M + F - 2*D)
135 +0.033 * sin(F + 2*D)
136 +0.017 * sin(2*M + F)
138 r += (-0.58 * cos(M - 2*D)
141 // FG_LOG(FG_GENERAL, FG_INFO, "Running moon update");
142 xg = r * cos(lonEcl) * cos(latEcl);
143 yg = r * sin(lonEcl) * cos(latEcl);
144 zg = r * sin(latEcl);
147 ye = yg * cos(ecl) -zg * sin(ecl);
148 ze = yg * sin(ecl) +zg * cos(ecl);
150 geoRa = atan2(ye, xe);
151 geoDec = atan2(ze, sqrt(xe*xe + ye*ye));
153 /* FG_LOG( FG_GENERAL, FG_INFO,
154 "(geocentric) geoRa = (" << (RAD_TO_DEG * geoRa)
155 << "), geoDec= (" << (RAD_TO_DEG * geoDec) << ")" ); */
158 // Given the moon's geocentric ra and dec, calculate its
159 // topocentric ra and dec. i.e. the position as seen from the
160 // surface of the earth, instead of the center of the earth
162 // First calculate the moon's parrallax, that is, the apparent size of the
163 // (equatorial) radius of the earth, as seen from the moon
164 mpar = asin ( 1 / r);
165 // FG_LOG( FG_GENERAL, FG_INFO, "r = " << r << " mpar = " << mpar );
166 // FG_LOG( FG_GENERAL, FG_INFO, "lat = " << f->get_Latitude() );
168 gclat = lat - 0.003358 *
169 sin (2 * DEG_TO_RAD * lat );
170 // FG_LOG( FG_GENERAL, FG_INFO, "gclat = " << gclat );
172 rho = 0.99883 + 0.00167 * cos(2 * DEG_TO_RAD * lat);
173 // FG_LOG( FG_GENERAL, FG_INFO, "rho = " << rho );
178 HA = lst - (3.8197186 * geoRa);
179 /* FG_LOG( FG_GENERAL, FG_INFO, "t->getLst() = " << t->getLst()
180 << " HA = " << HA ); */
182 g = atan (tan(gclat) / cos ((HA / 3.8197186)));
183 // FG_LOG( FG_GENERAL, FG_INFO, "g = " << g );
185 rightAscension = geoRa - mpar * rho * cos(gclat) * sin(HA) / cos (geoDec);
186 declination = geoDec - mpar * rho * sin (gclat) * sin (g - geoDec) / sin(g);
188 /* FG_LOG( FG_GENERAL, FG_INFO,
189 "Ra = (" << (RAD_TO_DEG *rightAscension)
190 << "), Dec= (" << (RAD_TO_DEG *declination) << ")" ); */