#include <simgear/compiler.h>
-#ifdef FG_HAVE_STD_INCLUDES
+#ifdef SG_HAVE_STD_INCLUDES
# include <cmath>
# include <cstdio>
# include <ctime>
#include <simgear/math/vector.hxx>
#include <Main/globals.hxx>
+#include <Main/viewer.hxx>
#include <Scenery/scenery.hxx>
#include <Time/light.hxx>
/*
* assuming the apparent orbit of the moon about the earth is circular,
* the rate at which the orbit progresses is given by RadsPerDay --
- * FG_2PI radians per orbit divided by 365.242191 days per year:
+ * SG_2PI radians per orbit divided by 365.242191 days per year:
*/
-#define RadsPerDay (FG_2PI/365.242191)
+#define RadsPerDay (SG_2PI/365.242191)
/*
* details of moon's apparent orbit at epoch 1990.0 (after
* Eccentricity (eccentricity of orbit) 0.016713
*/
-#define Epsilon_g (279.403303*(FG_2PI/360))
-#define OmegaBar_g (282.768422*(FG_2PI/360))
+#define Epsilon_g (279.403303*(SGD_2PI/360))
+#define OmegaBar_g (282.768422*(SGD_2PI/360))
#define Eccentricity (0.016713)
/*
* 1990.0 (computed as 23.440592 degrees according to the method given
* in duffett-smith, section 27)
*/
-#define MeanObliquity (23.440592*(FG_2PI/360))
+#define MeanObliquity (23.440592*(SGD_2PI/360))
/* static double solve_keplers_equation(double); */
/* static double moon_ecliptic_longitude(time_t); */
D = DaysSinceEpoch(ssue);
N = RadsPerDay * D;
- N = fmod(N, FG_2PI);
- if (N < 0) N += FG_2PI;
+ N = fmod(N, SG_2PI);
+ if (N < 0) N += SG_2PI;
M_moon = N + Epsilon_g - OmegaBar_g;
- if (M_moon < 0) M_moon += FG_2PI;
+ if (M_moon < 0) M_moon += SG_2PI;
E = solve_keplers_equation(M_moon);
v = 2 * atan(sqrt((1+Eccentricity)/(1-Eccentricity)) * tan(E/2));
/* lazy test to ensure gregorian calendar */
if (y < 1583) {
- FG_LOG( FG_EVENT, FG_ALERT,
+ SG_LOG( SG_EVENT, SG_ALERT,
"WHOOPS! Julian dates only valid for 1582 oct 15 or later" );
}
ecliptic_to_equatorial( globals->get_ephem()->get_moon()->getLon(),
0.0, &alpha, &delta );
- tmp = alpha - (FG_2PI/24)*GST(ssue);
- if (tmp < -FG_PI) {
- do tmp += FG_2PI;
- while (tmp < -FG_PI);
- } else if (tmp > FG_PI) {
- do tmp -= FG_2PI;
- while (tmp < -FG_PI);
+ tmp = alpha - (SGD_2PI/24)*GST(ssue);
+ if (tmp < -SGD_PI) {
+ do tmp += SGD_2PI;
+ while (tmp < -SGD_PI);
+ } else if (tmp > SGD_PI) {
+ do tmp -= SGD_2PI;
+ while (tmp < -SGD_PI);
}
*lon = tmp;
globals->get_ephem()->get_moon()->getLat(),
&alpha, &delta );
-// tmp = alpha - (FG_2PI/24)*GST(ssue);
- tmp = alpha - (FG_2PI/24)*gst;
- if (tmp < -FG_PI) {
- do tmp += FG_2PI;
- while (tmp < -FG_PI);
- } else if (tmp > FG_PI) {
- do tmp -= FG_2PI;
- while (tmp < -FG_PI);
+// tmp = alpha - (SG_2PI/24)*GST(ssue);
+ tmp = alpha - (SGD_2PI/24)*gst;
+ if (tmp < -SGD_PI) {
+ do tmp += SGD_2PI;
+ while (tmp < -SGD_PI);
+ } else if (tmp > SGD_PI) {
+ do tmp -= SGD_2PI;
+ while (tmp < -SGD_PI);
}
*lon = tmp;
// update the cur_time_params structure with the current moon position
void fgUpdateMoonPos( void ) {
fgLIGHT *l;
- FGViewerRPH *v;
+ FGViewer *v;
sgVec3 nup, nmoon;
Point3D p, rel_moonpos;
double dot, east_dot;
l = &cur_light_params;
SGTime *t = globals->get_time_params();
- v = (FGViewerRPH *)globals->get_current_view();
+ v = globals->get_current_view();
- FG_LOG( FG_EVENT, FG_INFO, " Updating Moon position" );
+ SG_LOG( SG_EVENT, SG_INFO, " Updating Moon position" );
// (not sure why there was two)
// fgMoonPosition(t->cur_time, &l->moon_lon, &moon_gd_lat);
p = Point3D( l->moon_lon, l->moon_gc_lat, sl_radius );
l->fg_moonpos = sgPolarToCart3d(p);
- FG_LOG( FG_EVENT, FG_INFO, " t->cur_time = " << t->get_cur_time() );
- FG_LOG( FG_EVENT, FG_INFO,
+ SG_LOG( SG_EVENT, SG_INFO, " t->cur_time = " << t->get_cur_time() );
+ SG_LOG( SG_EVENT, SG_INFO,
" Moon Geodetic lat = " << moon_gd_lat
<< " Geocentric lat = " << l->moon_gc_lat );
// << nmoon[2] << endl;
l->moon_angle = acos( sgScalarProductVec3( nup, nmoon ) );
- cout << "moon angle relative to current location = "
- << l->moon_angle << endl;
+ SG_LOG( SG_EVENT, SG_INFO, "moon angle relative to current location = "
+ << l->moon_angle );
// calculate vector to moon's position on the earth's surface
Point3D vp( v->get_view_pos()[0],
v->get_view_pos()[1],
v->get_view_pos()[2] );
- rel_moonpos = l->fg_moonpos - ( vp + scenery.center );
+ rel_moonpos = l->fg_moonpos - ( vp + scenery.get_center() );
sgSetVec3( to_moon, rel_moonpos.x(), rel_moonpos.y(), rel_moonpos.z() );
// printf( "Vector to moon = %.2f %.2f %.2f\n",
// to_moon[0], to_moon[1], to_moon[2]);
// v->surface_east. We do this so we can sort out the acos()
// ambiguity. I wish I could think of a more efficient way ... :-(
east_dot = sgScalarProductVec3( surface_to_moon, v->get_surface_east() );
- // cout << " East dot product = " << east_dot << endl;
+ // cout << " East dot product = " << east_dot << endl;
// calculate the angle between v->surface_to_moon and
// v->surface_south. this is how much we have to rotate the sky
l->moon_rotation = -acos(dot);
}
// cout << " Sky needs to rotate = " << angle << " rads = "
- // << angle * RAD_TO_DEG << " degrees." << endl;
+ // << angle * SGD_RADIANS_TO_DEGREES << " degrees." << endl;
}