コード例 #1
0
ファイル: uranus2.cpp プロジェクト: Bill-Gray/lunar
int main( const int argc, const char **argv)
{
    const int test_differences = (argc == 1 || argc == 3);
    const double jde = (argc == 1 ? 2451539.5 : atof( argv[1]));
    int nSat;                     // loop counter

    // Process each satellite in turn.

    setvbuf( stdout, NULL, _IONBF, 0);
    for (nSat=0; nSat<5; nSat++)
    {
        double dRect[6];               // satellite coordinates

        // Retrieve the coordinates of the satellite relative to the
        // centre of Saturn. These are equatorial coordinates for the
        // mean ecliptic and epoch of J2000.0.  Positions in AU,
        // velocities in AU/second.  Printed out in km and km/s.

        memset( dRect, 0, 6 * sizeof( double));
        gust86_posn( jde, nSat, dRect );

        if( test_differences)
            subtract_test_data( dRect, nSat, 0);
        printf( "%d: %14.6lf %14.6lf %14.6lf\n", nSat, dRect[0] * AU_IN_KM,
                dRect[1] * AU_IN_KM,
                dRect[2] * AU_IN_KM);
        if( test_differences)
            subtract_test_data( dRect + 3, nSat, 1);
        printf( "   %14.6lf %14.6lf %14.6lf\n", dRect[3] * AU_IN_KM,
                dRect[4] * AU_IN_KM,
                dRect[5] * AU_IN_KM);
    }
    return( 0);
}
コード例 #2
0
ファイル: uranus1.cpp プロジェクト: gerlache/MassMpCCD
int main( int argc, char **argv)
{
   const int test_differences = (argc == 1 || argc == 3);
   const double jde = (argc == 1 ? 2451539.5 : atof( argv[1]));
   int nSat;                     // loop counter
   const char *sat_names[5] = {
         "Ariel", "Umbriel", "Titania", "Oberon", "Miranda" };

   // Process each satellite in turn.

   for (nSat=0; nSat<5; nSat++)
   {
      double dRect[6];               // satellite coordinates

      // Retrieve the coordinates of the satellite relative to the
      // centre of Saturn. These are equatorial coordinates for the
      // mean ecliptic and epoch of J2000.0.  Positions in AU,
      // velocities in AU/second.  Printed out in km and km/s.

      gust86_posn( jde, nSat, dRect );
      if( test_differences)
         subtract_test_data( dRect, nSat, 0);
      printf( "%d %-8s: %14.6lf %14.6lf %14.6lf\n", nSat, sat_names[nSat],
                                               dRect[0] * AU_IN_KM,
                                               dRect[1] * AU_IN_KM,
                                               dRect[2] * AU_IN_KM);
      if( test_differences)
         subtract_test_data( dRect + 3, nSat, 1);
      printf( "            %14.6lf %14.6lf %14.6lf\n",
                                              dRect[3] * AU_IN_KM,
                                              dRect[4] * AU_IN_KM,
                                              dRect[5] * AU_IN_KM);
   }
   return( 0);
}