Removed unused SatelliteOrbit.*

Makefile

@@ -10,7 +10,6 @@ SOURCES=CoordGeodetic.cpp \
 	Julian.cpp \
 	Observer.cpp \
 	SGP4.cpp \
-	SatelliteOrbit.cpp \
         Timespan.cpp \
 	Tle.cpp \
 	Vector.cpp

Rewrite.vcxproj

@@ -81,7 +81,6 @@
     <ClCompile Include="Julian.cpp" />
     <ClCompile Include="Observer.cpp" />
     <ClCompile Include="RunTest.cpp" />
-    <ClCompile Include="SatelliteOrbit.cpp" />
     <ClCompile Include="SGP4.cpp" />
     <ClCompile Include="SolarPosition.cpp" />
     <ClCompile Include="Timespan.cpp" />
@@ -96,7 +95,6 @@
     <ClInclude Include="Julian.h" />
     <ClInclude Include="Observer.h" />
     <ClInclude Include="SatelliteException.h" />
-    <ClInclude Include="SatelliteOrbit.h" />
     <ClInclude Include="SGP4.h" />
     <ClInclude Include="SolarPosition.h" />
     <ClInclude Include="Timespan.h" />

Rewrite.vcxproj.filters

@@ -36,9 +36,6 @@
     <ClCompile Include="Timespan.cpp">
       <Filter>Source Files</Filter>
     </ClCompile>
-    <ClCompile Include="SatelliteOrbit.cpp">
-      <Filter>Source Files</Filter>
-    </ClCompile>
     <ClCompile Include="SGP4.cpp">
       <Filter>Source Files</Filter>
     </ClCompile>
@@ -80,9 +77,6 @@
     <ClInclude Include="Timespan.h">
       <Filter>Header Files</Filter>
     </ClInclude>
-    <ClInclude Include="SatelliteOrbit.h">
-      <Filter>Header Files</Filter>
-    </ClInclude>
     <ClInclude Include="SGP4.h">
       <Filter>Header Files</Filter>
     </ClInclude>

SatelliteOrbit.cpp

@@ -1,50 +0,0 @@
-#include "SatelliteOrbit.h"
-
-SatelliteOrbit::SatelliteOrbit(void) {
-}
-
-SatelliteOrbit::~SatelliteOrbit(void) {
-}
-
-void SatelliteOrbit::SetTle(const Tle& tle) {
-
-    sgp4_.SetTle(tle);
-}
-
-bool SatelliteOrbit::IsGeostationary() {
-
-    if (sgp4_.MeanMotion() == 0.0)
-        return true;
-
-    /*
-    radius of apogee
-    the distance from the centre of the planet to the point in the orbit furthest away from the planet
-     */
-    const double apogee_altitude = sgp4_.RecoveredSemiMajorAxis() * (1.0 + sgp4_.Eccentricity()) - Globals::XKMPER();
-
-    /*
-     * check if almost same speed as earth
-     * or altitude is over 35000 km
-     */
-    if (fabs(sgp4_.MeanMotion() - Globals::OMEGA_E()) < 0.0005 || apogee_altitude > 35000)
-        return true;
-    else
-        return false;
-}
-
-unsigned int SatelliteOrbit::GetOrbitNumber(const Julian& jul) const {
-
-    double diff = jul.SpanMin(sgp4_.Epoch());
-
-    return static_cast<unsigned int> (floor((sgp4_.MeanMotion() * 1440.0 / Globals::TWOPI() +
-            diff * sgp4_.BStar() * Globals::AE()) * diff +
-            sgp4_.MeanAnomoly() / Globals::TWOPI())) + sgp4_.OrbitNumber() - 1;
-}
-
-double SatelliteOrbit::Footprint(const double& altitude) {
-
-    if (altitude > 0)
-        return 2.0 * Globals::XKMPER() * acos(Globals::XKMPER() / (Globals::XKMPER() + altitude));
-    else
-        return 0.0;
-}

SatelliteOrbit.h

@@ -1,25 +0,0 @@
-#ifndef SATELLITEORBIT_H_
-#define SATELLITEORBIT_H_
-
-#include "Tle.h"
-#include "SGP4.h"
-
-class SatelliteOrbit {
-public:
-    SatelliteOrbit(void);
-    virtual ~SatelliteOrbit(void);
-
-    void SetTle(const Tle& tle);
-
-    bool IsGeostationary();
-
-    unsigned int GetOrbitNumber(const Julian& jul) const;
-
-    static double Footprint(const double& altitude);
-
-private:
-    SGP4 sgp4_;
-};
-
-#endif
-