X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=simgear%2Fephemeris%2Fstar.cxx;h=b36a9006bed85f488fcfaa53e720aaf8c51cb91c;hb=598b64fa9569c16878c904e344e2e2775e210c42;hp=01f20b729520b3977bbc36e7faaca63a93040cd8;hpb=82459a2802a939434f9fc5b88d2b2aea58f0043d;p=simgear.git

diff --git a/simgear/ephemeris/star.cxx b/simgear/ephemeris/star.cxx
index 01f20b72..b36a9006 100644
--- a/simgear/ephemeris/star.cxx
+++ b/simgear/ephemeris/star.cxx
@@ -15,19 +15,14 @@
  * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the GNU
  * Library General Public License for more details.
  *
- * You should have received a copy of the GNU Library General Public
- * License along with this library; if not, write to the
- * Free Software Foundation, Inc., 59 Temple Place - Suite 330,
- * Boston, MA  02111-1307, USA.
+ * 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., 51 Franklin Street, Fifth Floor, Boston, MA  02110-1301, USA.
  *
  * $Id$
  **************************************************************************/
 
-
-#ifdef __BORLANDC__
-#  define exception c_exception
-#endif
-#include <math.h>
+#include <cmath>
 
 #include <simgear/debug/logstream.hxx>
 
@@ -80,13 +75,13 @@ void Star::updatePosition(double mjd)
   double 
     actTime, eccAnom, 
     xv, yv, v, r,
-    xe, ye, ze, ecl;
+    xe, ecl;
 
   updateOrbElements(mjd);
   
-  actTime = fgCalcActTime(mjd);
-  ecl = DEG_TO_RAD * (23.4393 - 3.563E-7 * actTime); // Angle in Radians
-  eccAnom = fgCalcEccAnom(M, e);  // Calculate the eccentric Anomaly (also known as solving Kepler's equation)
+  actTime = sgCalcActTime(mjd);
+  ecl = SGD_DEGREES_TO_RADIANS * (23.4393 - 3.563E-7 * actTime); // Angle in Radians
+  eccAnom = sgCalcEccAnom(M, e);  // Calculate the eccentric Anomaly (also known as solving Kepler's equation)
   
   xv = cos(eccAnom) - e;
   yv = sqrt (1.0 - e*e) * sin(eccAnom);