* Eccentricity (eccentricity of orbit) 0.016713
*/
-#define Epsilon_g (279.403303*(SG_2PI/360))
-#define OmegaBar_g (282.768422*(SG_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*(SG_2PI/360))
+#define MeanObliquity (23.440592*(SGD_2PI/360))
/* static double solve_keplers_equation(double); */
/* static double moon_ecliptic_longitude(time_t); */
/* 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 - (SG_2PI/24)*GST(ssue);
+ tmp = alpha - (SGD_2PI/24)*GST(ssue);
if (tmp < -SGD_PI) {
- do tmp += SG_2PI;
+ do tmp += SGD_2PI;
while (tmp < -SGD_PI);
} else if (tmp > SGD_PI) {
- do tmp -= SG_2PI;
+ do tmp -= SGD_2PI;
while (tmp < -SGD_PI);
}
&alpha, &delta );
// tmp = alpha - (SG_2PI/24)*GST(ssue);
- tmp = alpha - (SG_2PI/24)*gst;
+ tmp = alpha - (SGD_2PI/24)*gst;
if (tmp < -SGD_PI) {
- do tmp += SG_2PI;
+ do tmp += SGD_2PI;
while (tmp < -SGD_PI);
} else if (tmp > SGD_PI) {
- do tmp -= SG_2PI;
+ do tmp -= SGD_2PI;
while (tmp < -SGD_PI);
}
SGTime *t = globals->get_time_params();
v = (FGViewerRPH *)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 ) );
- FG_LOG( FG_EVENT, FG_INFO, "moon angle relative to current location = "
+ 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
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;
}