X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=src%2FTime%2Fmoonpos.cxx;h=4c88c6c91b70f6d157cdca31383abe8710561918;hb=d4f92d6affa13d4f10a7a53367de9a511035a14b;hp=0fb907236d4742ad6f6f8db2dcf24470193cfd5d;hpb=f24b6a4098c79a1c47d6dfba97e959fb0e7c6d38;p=flightgear.git

diff --git a/src/Time/moonpos.cxx b/src/Time/moonpos.cxx
index 0fb907236..4c88c6c91 100644
--- a/src/Time/moonpos.cxx
+++ b/src/Time/moonpos.cxx
@@ -42,7 +42,7 @@
 
 #include <simgear/compiler.h>
 
-#ifdef FG_HAVE_STD_INCLUDES
+#ifdef SG_HAVE_STD_INCLUDES
 #  include <cmath>
 #  include <cstdio>
 #  include <ctime>
@@ -59,8 +59,10 @@
 #include <simgear/math/polar3d.hxx>
 #include <simgear/math/sg_geodesy.hxx>
 #include <simgear/math/vector.hxx>
+#include <simgear/timing/sg_time.hxx>
 
 #include <Main/globals.hxx>
+#include <Main/viewer.hxx>
 #include <Scenery/scenery.hxx>
 #include <Time/light.hxx>
 
@@ -85,10 +87,10 @@
 /*
  * 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
@@ -99,8 +101,8 @@
  * 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)
 
 /*
@@ -108,7 +110,7 @@
  * 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); */
@@ -149,11 +151,11 @@ static double moon_ecliptic_longitude(time_t ssue) {
     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));
@@ -200,7 +202,7 @@ static double julian_date(int y, int m, int d) {
 
     /* 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" );
     }
 
@@ -283,13 +285,13 @@ void fgMoonPosition(time_t ssue, double *lon, double *lat) {
 
     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;
@@ -317,14 +319,14 @@ static void fgMoonPositionGST(double gst, double *lon, double *lat) {
 			    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;
@@ -335,7 +337,7 @@ static void fgMoonPositionGST(double gst, double *lon, double *lat) {
 // 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;
@@ -350,9 +352,9 @@ void fgUpdateMoonPos( void ) {
 
     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);
@@ -363,8 +365,8 @@ void fgUpdateMoonPos( void ) {
     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 );
 
@@ -391,14 +393,14 @@ void fgUpdateMoonPos( void ) {
     //      << 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 + globals->get_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]);
@@ -421,7 +423,7 @@ void fgUpdateMoonPos( void ) {
     // 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
@@ -435,7 +437,7 @@ void fgUpdateMoonPos( void ) {
 	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;
 }