simgear/Scenery/sun.c

62 lines
1.9 KiB
C

/**************************************************************************
* 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.
/*
*/