X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=simgear%2Fephemeris%2FcelestialBody.hxx;h=e555deef54078e7e1483a1d88bd20ba84bcc83cd;hb=598b64fa9569c16878c904e344e2e2775e210c42;hp=9311b78c1d5aa34eab72cace03e3b417f085fe04;hpb=9a211af659e744ffb2f19983761916a9f1a024ea;p=simgear.git

diff --git a/simgear/ephemeris/celestialBody.hxx b/simgear/ephemeris/celestialBody.hxx
index 9311b78c..e555deef 100644
--- a/simgear/ephemeris/celestialBody.hxx
+++ b/simgear/ephemeris/celestialBody.hxx
@@ -15,10 +15,9 @@
  * 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.
  *
  * $Id$
  **************************************************************************/
@@ -27,9 +26,9 @@
 #ifndef _CELESTIALBODY_H_
 #define _CELESTIALBODY_H_
 
-#ifndef __cplusplus                                                          
+#ifndef __cplusplus
 # error This library requires C++
-#endif                                   
+#endif
 
 
 #include <simgear/constants.h>
@@ -82,142 +81,24 @@ public:
   double getRightAscension();
   double getDeclination();
   double getMagnitude();
-  double getLon();
-  double getLat(); 
+  double getLon() const;
+  double getLat() const; 
   void updatePosition(double mjd, Star *ourSun);
 };
 
-/*****************************************************************************
- * inline CelestialBody::CelestialBody
- * public constructor for a generic celestialBody object.
- * initializes the 6 primary orbital elements. The elements are:
- * N: longitude of the ascending node
- * i: inclination to the ecliptic
- * w: argument of perihelion
- * a: semi-major axis, or mean distance from the sun
- * e: eccenticity
- * M: mean anomaly
- * Each orbital element consists of a constant part and a variable part that 
- * gradually changes over time. 
- *
- * Argumetns:
- * the 13 arguments to the constructor constitute the first, constant 
- * ([NiwaeM]f) and the second variable ([NiwaeM]s) part of the orbital 
- * elements. The 13th argument is the current time. Note that the inclination
- * is written with a capital (If, Is), because 'if' is a reserved word in the 
- * C/C++ programming language.
- ***************************************************************************/ 
-inline CelestialBody::CelestialBody(double Nf, double Ns,
-				    double If, double Is,
-				    double wf, double ws,
-				    double af, double as,
-				    double ef, double es,
-				    double Mf, double Ms, double mjd)
-{
-  NFirst = Nf;     NSec = Ns;
-  iFirst = If;     iSec = Is;
-  wFirst = wf;     wSec = ws;
-  aFirst = af;     aSec = as;
-  eFirst = ef;     eSec = es;
-  MFirst = Mf;     MSec = Ms;
-  updateOrbElements(mjd);
-};
-
-inline CelestialBody::CelestialBody(double Nf, double Ns,
-				    double If, double Is,
-				    double wf, double ws,
-				    double af, double as,
-				    double ef, double es,
-				    double Mf, double Ms)
-{
-  NFirst = Nf;     NSec = Ns;
-  iFirst = If;     iSec = Is;
-  wFirst = wf;     wSec = ws;
-  aFirst = af;     aSec = as;
-  eFirst = ef;     eSec = es;
-  MFirst = Mf;     MSec = Ms;
-};
-
-/****************************************************************************
- * inline void CelestialBody::updateOrbElements(double mjd)
- * given the current time, this private member calculates the actual 
- * orbital elements
- *
- * Arguments: double mjd: the current modified julian date:
- *
- * return value: none
- ***************************************************************************/
-inline void CelestialBody::updateOrbElements(double mjd)
-{
-  double actTime = sgCalcActTime(mjd);
-   M = DEG_TO_RAD * (MFirst + (MSec * actTime));
-   w = DEG_TO_RAD * (wFirst + (wSec * actTime));
-   N = DEG_TO_RAD * (NFirst + (NSec * actTime));
-   i = DEG_TO_RAD * (iFirst + (iSec * actTime));
-   e = eFirst + (eSec * actTime);
-   a = aFirst + (aSec * actTime);
-}
-/*****************************************************************************
- * inline double CelestialBody::sgCalcActTime(double mjd)
- * this private member function returns the offset in days from the epoch for
- * wich the orbital elements are calculated (Jan, 1st, 2000).
- * 
- * Argument: the current time
- *
- * return value: the (fractional) number of days until Jan 1, 2000.
- ****************************************************************************/
-inline double CelestialBody::sgCalcActTime(double mjd)
-{
-  return (mjd - 36523.5);
-}
-
-/*****************************************************************************
- * inline void CelestialBody::getPos(double* ra, double* dec)
- * gives public access to Right Ascension and declination
- *
- ****************************************************************************/
-inline void CelestialBody::getPos(double* ra, double* dec)
-{
-  *ra  = rightAscension;
-  *dec = declination;
-}
-
-/*****************************************************************************
- * inline void CelestialBody::getPos(double* ra, double* dec, double* magnitude
- * gives public acces to the current Right ascension, declination, and 
- * magnitude
- ****************************************************************************/
-inline void CelestialBody::getPos(double* ra, double* dec, double* magn)
-{
-  *ra = rightAscension;
-  *dec = declination;
-  *magn = magnitude;
-}
-
 inline double CelestialBody::getRightAscension() { return rightAscension; }
 inline double CelestialBody::getDeclination() { return declination; }
 inline double CelestialBody::getMagnitude() { return magnitude; }
 
-inline double CelestialBody::getLon()
+inline double CelestialBody::getLon() const
 {
   return lonEcl;
 }
 
-inline double CelestialBody::getLat()
+inline double CelestialBody::getLat() const
 {
   return latEcl;
 }
 
 #endif // _CELESTIALBODY_H_
 
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