Cmake: restore its original name to the ephemeris library

[simgear.git] / simgear / ephemeris / saturn.cxx

diff --git a/simgear/ephemeris/saturn.cxx b/simgear/ephemeris/saturn.cxx
index 981b67f5f0b6d116fb7c3ef90f383fc60ea0ad4c..0038a290136dadafd0112fb1235e4d58738dee06 100644 (file)
--- a/simgear/ephemeris/saturn.cxx
+++ b/simgear/ephemeris/saturn.cxx
@@ -5,26 +5,23 @@
  * September 1998. This code is based upon algorithms and data kindly 
  * provided by Mr. Paul Schlyter. (pausch@saaf.se). 
  *
- * 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 library is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Library 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
+ * This library 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.
+ * Library 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.
+ * Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA  02110-1301, USA.
  *
  * $Id$
  **************************************************************************/
 
-#ifdef __BORLANDC__
-#  define exception c_exception
-#endif
 #include <math.h>
 
 #include "saturn.hxx"
@@ -66,7 +63,7 @@ void Saturn::updatePosition(double mjd, Star *ourSun)
 {
   CelestialBody::updatePosition(mjd, ourSun);
   
-  double actTime = fgCalcActTime(mjd);
+  double actTime = sgCalcActTime(mjd);
   double ir = 0.4897394;
   double Nr = 2.9585076 + 6.6672E-7*actTime;
   double B = asin (sin(declination) * cos(ir) -