Initial revision of code contributed by Durk Talsma.
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171
Scenery/moon.c
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171
Scenery/moon.c
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/**************************************************************************
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* moon.c
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*
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* This program is free software; you can redistribute it and/or
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* modify it under the terms of the GNU General Public License as
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* published by the Free Software Foundation; either version 2 of the
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* License, or (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful, but
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* WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
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* General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with this program; if not, write to the Free Software
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* Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
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*
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* $Id$
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* (Log is kept at end of this file)
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**************************************************************************/
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#include <math.h>
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#include <GL/glut.h>
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#include "orbits.h"
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#include "moon.h"
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#include "../Time/fg_time.h"
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#include "../GLUT/views.h"
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/* #include "../Aircraft/aircraft.h"*/
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#include "../general.h"
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static GLint moon;
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struct CelestialCoord fgCalculateMoon(struct OrbElements params,
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struct OrbElements sunParams,
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struct fgTIME t)
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{
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struct CelestialCoord
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result;
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double
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eccAnom, ecl, lonecl, latecl, actTime,
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xv, yv, v, r, xh, yh, zh, xg, yg, zg, xe, ye, ze,
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Ls, Lm, D, F;
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/* calculate the angle between ecliptic and equatorial coordinate system */
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actTime = fgCalcActTime(t);
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ecl = fgDegToRad(23.4393 - 3.563E-7 * actTime); // in radians of course
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/* calculate the eccentric anomaly */
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eccAnom = fgCalcEccAnom(params.M, params.e);
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/* calculate the moon's distance (d) and true anomaly (v) */
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xv = params.a * ( cos(eccAnom) - params.e);
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yv = params.a * ( sqrt(1.0 - params.e*params.e) * sin(eccAnom));
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v =atan2(yv, xv);
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r = sqrt(xv*xv + yv*yv);
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/* estimate the geocentric rectangular coordinates here */
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xh = r * (cos(params.N) * cos(v + params.w) - sin(params.N) * sin(v + params.w) * cos(params.i));
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yh = r * (sin(params.N) * cos(v + params.w) + cos(params.N) * sin(v + params.w) * cos(params.i));
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zh = r * (sin(v + params.w) * sin(params.i));
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/* calculate the ecliptic latitude and longitude here */
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lonecl = atan2( yh, xh);
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latecl = atan2( zh, sqrt( xh*xh + yh*yh));
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/* calculate a number of perturbations */
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Ls = sunParams.M + sunParams.w;
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Lm = params.M + params.w + params.N;
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D = Lm - Ls;
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F = Lm - params.N;
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lonecl += fgDegToRad(
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- 1.274 * sin (params.M - 2*D) // the Evection
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+ 0.658 * sin (2 * D) // the Variation
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- 0.186 * sin (sunParams.M) // the yearly variation
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- 0.059 * sin (2*params.M - 2*D)
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- 0.057 * sin (params.M - 2*D + sunParams.M)
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+ 0.053 * sin (params.M + 2*D)
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+ 0.046 * sin (2*D - sunParams.M)
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+ 0.041 * sin (params.M - sunParams.M)
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- 0.035 * sin (D) // the Parallactic Equation
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- 0.031 * sin (params.M + sunParams.M)
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- 0.015 * sin (2*F - 2*D)
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+ 0.011 * sin (params.M - 4*D)
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); /* Pheeuuwwww */
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latecl += fgDegToRad(
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- 0.173 * sin (F - 2*D)
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- 0.055 * sin (params.M - F - 2*D)
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- 0.046 * sin (params.M + F - 2*D)
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+ 0.033 * sin (F + 2*D)
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+ 0.017 * sin (2 * params.M + F)
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); /* Yep */
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r += (
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- 0.58 * cos(params.M - 2*D)
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- 0.46 * cos(2*D)
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);
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xg = r * cos(lonecl) * cos(latecl);
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yg = r * sin(lonecl) * cos(latecl);
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zg = r * sin(latecl);
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xe = xg;
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ye = yg * cos(ecl) - zg * sin(ecl);
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ze = yg * sin(ecl) + zg * cos(ecl);
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result.RightAscension = atan2(ye, xe);
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result.Declination = atan2(ze, sqrt(xe*xe + ye*ye));
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return result;
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}
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void fgMoonInit()
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{
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struct CelestialCoord
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moonPos;
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moon = glGenLists(1);
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glNewList(moon, GL_COMPILE );
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glBegin( GL_POINTS );
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moonPos = fgCalculateMoon(pltOrbElements[1], pltOrbElements[0], cur_time_params);
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printf("Moon found at %f (ra), %f (dec)\n", moonPos.RightAscension, moonPos.Declination);
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/* give the moon a temporary color, for testing purposes */
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glColor3f( 0.0, 1.0, 0.0);
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glVertex3f( 190000.0 * cos(moonPos.RightAscension) * cos(moonPos.Declination),
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190000.0 * sin(moonPos.RightAscension) * cos(moonPos.Declination),
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190000.0 * sin(moonPos.Declination) );
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glEnd();
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glEndList();
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}
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void fgMoonRender()
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{
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double angle;
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static double warp = 0;
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struct VIEW *v;
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struct fgTIME *t;
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t = &cur_time_params;
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v = ¤t_view;
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glDisable( GL_FOG );
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glDisable( GL_LIGHTING );
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glPushMatrix();
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glTranslatef( v->view_pos.x, v->view_pos.y, v->view_pos.z );
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angle = t->gst * 15.0; /* 15 degrees per hour rotation */
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/* warp += 1.0; */
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/* warp = 15.0; */
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warp = 0.0;
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glRotatef( (angle+warp), 0.0, 0.0, -1.0 );
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printf("Rotating moon by %.2f degrees + %.2f degrees\n",angle,warp);
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glCallList(moon);
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glPopMatrix();
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glEnable( GL_LIGHTING );
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glEnable( GL_FOG );
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}
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/* $Log$
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/* Revision 1.1 1997/10/25 03:16:08 curt
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/* Initial revision of code contributed by Durk Talsma.
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/*
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*/
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54
Scenery/moon.h
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54
Scenery/moon.h
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@ -0,0 +1,54 @@
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/**************************************************************************
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* moon.h
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*
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* Written 1997 by Durk Talsma, started October, 1997.
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*
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* This program is free software; you can redistribute it and/or
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* modify it under the terms of the GNU General Public License as
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* published by the Free Software Foundation; either version 2 of the
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* License, or (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful, but
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* WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
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* General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with this program; if not, write to the Free Software
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* Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
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*
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* $Id$
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* (Log is kept at end of this file)
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**************************************************************************/
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#ifndef _MOON_H_
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#define _MOON_H_
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#include "orbits.h"
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#include "../Time/fg_time.h"
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/* Initialize the Moon Display management Subsystem */
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void fgMoonInit();
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/* Draw the Stars */
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void fgMoonRender();
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struct CelestialCoord fgCalculateMoon(struct OrbElements Params,
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struct OrbElements sunParams,
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struct fgTIME t);
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extern struct OrbElements pltOrbElements[9];
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#endif /* _MOON_H_ */
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/* $Log$
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/* Revision 1.1 1997/10/25 03:16:09 curt
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/* Initial revision of code contributed by Durk Talsma.
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/*
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*/
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170
Scenery/orbits.c
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170
Scenery/orbits.c
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/**************************************************************************
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* orbits.c - calculates the orbital elements of the sun, moon and planets.
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* For inclusion in flight gear
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*
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* Written 1997 by Durk Talsma, started October 19, 1997.
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*
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* This program is free software; you can redistribute it and/or
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* modify it under the terms of the GNU General Public License as
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* published by the Free Software Foundation; either version 2 of the
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* License, or (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful, but
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* WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
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* General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with this program; if not, write to the Free Software
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* Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
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*
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* $Id$
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* (Log is kept at end of this file)
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**************************************************************************/
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#include <string.h>
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#include "orbits.h"
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#include "../general.h"
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#include "../Time/fg_time.h"
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struct OrbElements pltOrbElements[9];
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double fgCalcActTime(struct fgTIME t)
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{
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double
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actTime, UT;
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int year;
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/* a hack. This one introduces the 2000 problem into the program */
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year = t.gmt->tm_year + 1900;
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/* calculate the actual time */
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actTime = 367 * year - 7 *
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(year + (t.gmt->tm_mon + 9) / 12) / 4 + 275 *
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t.gmt->tm_mon / 9 + t.gmt->tm_mday - 730530;
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UT = t.gmt->tm_hour + ((double) t.gmt->tm_min / 60);
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/*printf("UT = %f\n", UT); */
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actTime += (UT / 24.0);
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printf("current day = %f\t", actTime);
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printf("GMT = %d, %d, %d, %d, %d, %d\n", year, t.gmt->tm_mon, t.gmt->tm_mday,
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t.gmt->tm_hour, t.gmt->tm_min, t.gmt->tm_sec);
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return actTime;
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}
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/* convert degrees to radians */
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double fgDegToRad(double angle)
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{
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return (angle * PIOVER180);
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}
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double fgCalcEccAnom(double M, double e)
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{
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double
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eccAnom, E0, E1, diff;
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eccAnom = M + e * sin(M) * (1.0 + e * cos(M));
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/* iterate to achieve a greater precision for larger eccentricities */
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if (e > 0.05)
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{
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E0 = eccAnom;
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do
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{
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E1 = E0 - (E0 - e * sin(E0) - M) / (1 - e * cos(E0));
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diff = abs(E0 - E1);
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E0 = E1;
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}
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while (diff > fgDegToRad(0.001));
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return E0;
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}
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return eccAnom;
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}
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void fgReadOrbElements(struct OrbElements *dest, FILE *src)
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{
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char line[256];
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int i,j;
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j = 0;
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do
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{
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fgets(line, 256,src);
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for (i = 0; i < 256; i++)
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{
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if (line[i] == '#')
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line[i] = 0;
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}
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/*printf("Reading line %d\n", j++); */
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}
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while (!(strlen(line)));
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sscanf(line, "%lf,%lf,%lf,%lf,%lf,%lf,%lf,%lf,%lf,%lf,%lf,%lf\n",
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&dest->NFirst, &dest->NSec,
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&dest->iFirst, &dest->iSec,
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&dest->wFirst, &dest->wSec,
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&dest->aFirst, &dest->aSec,
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&dest->eFirst, &dest->eSec,
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&dest->MFirst, &dest->MSec);
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}
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void fgSolarSystemInit(struct fgTIME t)
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{
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struct GENERAL *g;
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char path[80];
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int i;
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FILE *data;
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/* build the full path name to the orbital elements database file */
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g = &general;
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path[0] = '\0';
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strcat(path, g->root_dir);
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strcat(path, "/Scenery/");
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strcat(path, "planets.dat");
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if ( (data = fopen(path, "r")) == NULL )
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{
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printf("Cannot open data file: '%s'\n", path);
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return;
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}
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printf("reading datafile %s", path);
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/* for all the objects... */
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for (i = 0; i < 9; i ++)
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{
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/* ...read from the data file ... */
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fgReadOrbElements(&pltOrbElements[i], data);
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/* ...and calculate the actual values */
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fgSolarSystemUpdate(&pltOrbElements[i], t);
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}
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}
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void fgSolarSystemUpdate(struct OrbElements *planet, struct fgTIME t)
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{
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double
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actTime;
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actTime = fgCalcActTime(t);
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/* calculate the actual orbital elements */
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planet->M = fgDegToRad(planet->MFirst + (planet->MSec * actTime)); // angle in radians
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planet->w = fgDegToRad(planet->wFirst + (planet->wSec * actTime)); // angle in radians
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planet->N = fgDegToRad(planet->NFirst + (planet->NSec * actTime)); // angle in radians
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planet->i = fgDegToRad(planet->iFirst + (planet->iSec * actTime)); // angle in radians
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planet->e = planet->eFirst + (planet->eSec * actTime);
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planet->a = planet->aFirst + (planet->aSec * actTime);
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}
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/* $Log$
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/* Revision 1.1 1997/10/25 03:16:10 curt
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/* Initial revision of code contributed by Durk Talsma.
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/*
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*/
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85
Scenery/orbits.h
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85
Scenery/orbits.h
Normal file
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@ -0,0 +1,85 @@
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/**************************************************************************
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* orbits.h - calculates the orbital elements of the sun, moon and planets.
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* For inclusion in flight gear
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*
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* Written 1997 by Durk Talsma, started October 19, 1997.
|
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*
|
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* This program is free software; you can redistribute it and/or
|
||||
* modify it under the terms of the GNU General Public License as
|
||||
* published by the Free Software Foundation; either version 2 of the
|
||||
* License, or (at your option) any later version.
|
||||
*
|
||||
* This program is distributed in the hope that it will be useful, but
|
||||
* WITHOUT ANY WARRANTY; without even the implied warranty of
|
||||
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
|
||||
* General Public License for more details.
|
||||
*
|
||||
* You should have received a copy of the GNU General Public License
|
||||
* along with this program; if not, write to the Free Software
|
||||
* Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
|
||||
*
|
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* $Id$
|
||||
* (Log is kept at end of this file)
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**************************************************************************/
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#ifndef ORBITS_H
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#define ORBITS_H
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#include <stdio.h>
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#include <math.h>
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#include "../Time/fg_time.h"
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#define STANDARDEPOCH 2000
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#define PIOVER180 1.74532925199433E-002
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struct SunPos {
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double xs;
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double ys;
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};
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struct OrbElements {
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double NFirst; /* longitude of the ascending node first part */
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double NSec; /* longitude of the ascending node second part */
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double iFirst; /* inclination to the ecliptic first part */
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double iSec; /* inclination to the ecliptic second part */
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double wFirst; /* first part of argument of perihelion */
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double wSec; /* second part of argument of perihelion */
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double aFirst; /* semimayor axis first part*/
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double aSec; /* semimayor axis second part */
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double eFirst; /* eccentricity first part */
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double eSec; /* eccentricity second part */
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double MFirst; /* Mean anomaly first part */
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double MSec; /* Mean anomaly second part */
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double N, i, w, a, e, M; /* the resultant orbital elements, obtained from the former */
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};
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struct CelestialCoord {
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double RightAscension;
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double Declination;
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double distance;
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};
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double fgDegToRad(double angle);
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double fgCalcEccAnom(double M, double e);
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double fgCalcActTime(struct fgTIME t);
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||||
|
||||
void fgReadOrbElements(struct OrbElements *dest, FILE *src);
|
||||
void fgSolarSystemInit(struct fgTIME t);
|
||||
void fgSolarSystemUpdate(struct OrbElements *planets, struct fgTIME t);
|
||||
|
||||
|
||||
#endif /* ORBITS_H */
|
||||
|
||||
|
||||
/* $Log$
|
||||
/* Revision 1.1 1997/10/25 03:16:10 curt
|
||||
/* Initial revision of code contributed by Durk Talsma.
|
||||
/*
|
||||
*/
|
||||
91
Scenery/planets.c
Normal file
91
Scenery/planets.c
Normal file
|
|
@ -0,0 +1,91 @@
|
|||
/**************************************************************************
|
||||
* planets.c
|
||||
*
|
||||
* Written 1997 by Durk Talsma, started October, 1997. For the flight gear
|
||||
* project.
|
||||
*
|
||||
* This program is free software; you can redistribute it and/or
|
||||
* modify it under the terms of the GNU General Public License as
|
||||
* published by the Free Software Foundation; either version 2 of the
|
||||
* License, or (at your option) any later version.
|
||||
*
|
||||
* This program is distributed in the hope that it will be useful, but
|
||||
* WITHOUT ANY WARRANTY; without even the implied warranty of
|
||||
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
|
||||
* General Public License for more details.
|
||||
*
|
||||
* You should have received a copy of the GNU General Public License
|
||||
* along with this program; if not, write to the Free Software
|
||||
* Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
|
||||
*
|
||||
* $Id$
|
||||
* (Log is kept at end of this file)
|
||||
**************************************************************************/
|
||||
|
||||
|
||||
#include "../Time/fg_time.h"
|
||||
#include "orbits.h"
|
||||
#include "planets.h"
|
||||
#include "sun.h"
|
||||
|
||||
|
||||
struct CelestialCoord fgCalculatePlanet(struct OrbElements planet,
|
||||
struct OrbElements sun,
|
||||
struct fgTIME t)
|
||||
{
|
||||
struct CelestialCoord
|
||||
result;
|
||||
|
||||
struct SunPos
|
||||
SolarPosition;
|
||||
|
||||
double
|
||||
eccAnom, r, v, ecl, actTime,
|
||||
xv, yv, xh, yh, zh, xg, yg, zg, xe, ye, ze;
|
||||
|
||||
actTime = fgCalcActTime(t);
|
||||
/* calculate the angle between ecliptic and equatorial coordinate system */
|
||||
ecl = fgDegToRad(23.4393 - 3.563E-7 * actTime);
|
||||
|
||||
|
||||
/* calculate the eccentric anomaly */
|
||||
eccAnom = fgCalcEccAnom(planet.M, planet.e);
|
||||
|
||||
/* calculate the planets distance (r) and true anomaly (v) */
|
||||
xv = planet.a * (cos(eccAnom) - planet.e);
|
||||
yv = planet.a * (sqrt(1.0 - planet.e*planet.e) * sin(eccAnom));
|
||||
v = atan2(yv, xv);
|
||||
r = sqrt ( xv*xv + yv*yv);
|
||||
|
||||
/* calculate the planets position in 3-dimensional space */
|
||||
xh = r * ( cos(planet.N) * cos(v+planet.w) - sin(planet.N) * sin(v+planet.w) * cos(planet.i));
|
||||
yh = r * ( sin(planet.N) * cos(v+planet.w) + cos(planet.N) * sin(v+planet.w) * cos(planet.i));
|
||||
zh = r * ( sin(v+planet.w) * sin(planet.i));
|
||||
|
||||
/* calculate the ecleptic longitude and latitude */
|
||||
|
||||
/*
|
||||
lonecl = atan2(yh, xh);
|
||||
latecl = atan2(zh, sqrt ( xh*xh + yh*yh));
|
||||
*/
|
||||
/* calculate the solar position */
|
||||
|
||||
SolarPosition = fgCalcSunPos(sun);
|
||||
xg = xh + SolarPosition.xs;
|
||||
yg = yh + SolarPosition.ys;
|
||||
zg = zh;
|
||||
|
||||
xe = xg;
|
||||
ye = yg * cos(ecl) - zg * sin(ecl);
|
||||
ze = yg * sin(ecl) + zg * cos(ecl);
|
||||
result.RightAscension = atan2(ye,xe);
|
||||
result.Declination = atan2(ze, sqrt(xe*xe + ye*ye));
|
||||
return result;
|
||||
}
|
||||
|
||||
|
||||
/* $Log$
|
||||
/* Revision 1.1 1997/10/25 03:16:10 curt
|
||||
/* Initial revision of code contributed by Durk Talsma.
|
||||
/*
|
||||
*/
|
||||
41
Scenery/planets.h
Normal file
41
Scenery/planets.h
Normal file
|
|
@ -0,0 +1,41 @@
|
|||
/**************************************************************************
|
||||
* planets.h
|
||||
*
|
||||
* Written 1997 by Durk Talsma, started October, 1997. For the flight gear
|
||||
* project.
|
||||
*
|
||||
* This program is free software; you can redistribute it and/or
|
||||
* modify it under the terms of the GNU General Public License as
|
||||
* published by the Free Software Foundation; either version 2 of the
|
||||
* License, or (at your option) any later version.
|
||||
*
|
||||
* This program is distributed in the hope that it will be useful, but
|
||||
* WITHOUT ANY WARRANTY; without even the implied warranty of
|
||||
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
|
||||
* General Public License for more details.
|
||||
*
|
||||
* You should have received a copy of the GNU General Public License
|
||||
* along with this program; if not, write to the Free Software
|
||||
* Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
|
||||
*
|
||||
* $Id$
|
||||
* (Log is kept at end of this file)
|
||||
**************************************************************************/
|
||||
|
||||
|
||||
#ifndef PLANETS_H
|
||||
#define PLANETS_H
|
||||
|
||||
|
||||
struct CelestialCoord fgCalculatePlanet(struct OrbElements planet,
|
||||
struct OrbElements sun,
|
||||
struct fgTIME t);
|
||||
|
||||
#endif /* PLANETS_H */
|
||||
|
||||
|
||||
/* $Log$
|
||||
/* Revision 1.1 1997/10/25 03:16:11 curt
|
||||
/* Initial revision of code contributed by Durk Talsma.
|
||||
/*
|
||||
*/
|
||||
61
Scenery/sun.c
Normal file
61
Scenery/sun.c
Normal file
|
|
@ -0,0 +1,61 @@
|
|||
/**************************************************************************
|
||||
* sun.c
|
||||
*
|
||||
* Written 1997 by Durk Talsma, started October, 1997. For the flight gear
|
||||
* project.
|
||||
*
|
||||
* This program is free software; you can redistribute it and/or
|
||||
* modify it under the terms of the GNU General Public License as
|
||||
* published by the Free Software Foundation; either version 2 of the
|
||||
* License, or (at your option) any later version.
|
||||
*
|
||||
* This program is distributed in the hope that it will be useful, but
|
||||
* WITHOUT ANY WARRANTY; without even the implied warranty of
|
||||
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
|
||||
* General Public License for more details.
|
||||
*
|
||||
* You should have received a copy of the GNU General Public License
|
||||
* along with this program; if not, write to the Free Software
|
||||
* Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
|
||||
*
|
||||
* $Id$
|
||||
* (Log is kept at end of this file)
|
||||
**************************************************************************/
|
||||
|
||||
|
||||
#include "../Time/fg_time.h"
|
||||
#include "orbits.h"
|
||||
|
||||
struct SunPos fgCalcSunPos(struct OrbElements params)
|
||||
{
|
||||
double
|
||||
EccAnom, lonSun,
|
||||
xv, yv, v, r;
|
||||
struct SunPos
|
||||
solarPosition;
|
||||
|
||||
/* calculate the eccentric anomaly */
|
||||
EccAnom = fgCalcEccAnom(params.M, params.e);
|
||||
|
||||
/* calculate the Suns distance (r) and its true anomaly (v) */
|
||||
xv = cos(EccAnom) - params.e;
|
||||
yv = sqrt(1.0 - params.e*params.e) * sin(EccAnom);
|
||||
v = atan2(yv, xv);
|
||||
r = sqrt(xv*xv + yv*yv);
|
||||
|
||||
/* calculate the the Suns true longitude (lonsun) */
|
||||
lonSun = v + params.w;
|
||||
|
||||
/* convert true longitude and distance to ecliptic rectangular geocentric
|
||||
coordinates (xs, ys) */
|
||||
solarPosition.xs = r * cos(lonSun);
|
||||
solarPosition.ys = r * sin(lonSun);
|
||||
return solarPosition;
|
||||
}
|
||||
|
||||
|
||||
/* $Log$
|
||||
/* Revision 1.1 1997/10/25 03:16:11 curt
|
||||
/* Initial revision of code contributed by Durk Talsma.
|
||||
/*
|
||||
*/
|
||||
40
Scenery/sun.h
Normal file
40
Scenery/sun.h
Normal file
|
|
@ -0,0 +1,40 @@
|
|||
/**************************************************************************
|
||||
* sun.h
|
||||
*
|
||||
* Written 1997 by Durk Talsma, started October, 1997. For the flight gear
|
||||
* project.
|
||||
*
|
||||
* This program is free software; you can redistribute it and/or
|
||||
* modify it under the terms of the GNU General Public License as
|
||||
* published by the Free Software Foundation; either version 2 of the
|
||||
* License, or (at your option) any later version.
|
||||
*
|
||||
* This program is distributed in the hope that it will be useful, but
|
||||
* WITHOUT ANY WARRANTY; without even the implied warranty of
|
||||
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
|
||||
* General Public License for more details.
|
||||
*
|
||||
* You should have received a copy of the GNU General Public License
|
||||
* along with this program; if not, write to the Free Software
|
||||
* Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
|
||||
*
|
||||
* $Id$
|
||||
* (Log is kept at end of this file)
|
||||
**************************************************************************/
|
||||
|
||||
|
||||
#ifndef SUN_H
|
||||
#define SUN_H
|
||||
|
||||
|
||||
struct SunPos fgCalcSunPos(struct OrbElements sunParams);
|
||||
|
||||
|
||||
#endif /* SUN_H */
|
||||
|
||||
|
||||
/* $Log$
|
||||
/* Revision 1.1 1997/10/25 03:16:12 curt
|
||||
/* Initial revision of code contributed by Durk Talsma.
|
||||
/*
|
||||
*/
|
||||
Loading…
Reference in a new issue