Index: trunk/BNC/RTCM3/ephemeris.cpp
===================================================================
--- trunk/BNC/RTCM3/ephemeris.cpp	(revision 2770)
+++ trunk/BNC/RTCM3/ephemeris.cpp	(revision 2771)
@@ -305,2 +305,126 @@
   _xv(6) = _z_velocity * 1.e3; 
 }
+
+// Set Galileo Satellite Position
+////////////////////////////////////////////////////////////////////////////
+void t_ephGal::set(const galileoephemeris* ee) {
+  ostringstream prn;
+  prn << 'E' << setfill('0') << setw(2) << ee->satellite;
+
+  _prn = prn.str();
+
+  _GPSweek  = ee->Week;
+  _GPSweeks = ee->TOE;
+
+  _TOC    = ee->TOC;
+  _TOE    = ee->TOE;
+  _IODnav = ee->IODnav;             
+
+  _clock_bias      = ee->clock_bias     ;
+  _clock_drift     = ee->clock_drift    ;
+  _clock_driftrate = ee->clock_driftrate;
+
+  _Crs      = ee->Crs;
+  _Delta_n  = ee->Delta_n;
+  _M0       = ee->M0;
+  _Cuc      = ee->Cuc;
+  _e        = ee->e;
+  _Cus      = ee->Cus;
+  _sqrt_A   = ee->sqrt_A;
+  _Cic      = ee->Cic;
+  _OMEGA0   = ee->OMEGA0;
+  _Cis      = ee->Cis;
+  _i0       = ee->i0;
+  _Crc      = ee->Crc;
+  _omega    = ee->omega;
+  _OMEGADOT = ee->OMEGADOT;
+  _IDOT     = ee->IDOT;
+}
+
+// Compute Galileo Satellite Position (virtual)
+////////////////////////////////////////////////////////////////////////////
+void t_ephGal::position(int GPSweek, double GPSweeks, 
+			double* xc,
+			double* vv) const {
+
+  static const double secPerWeek = 7 * 86400.0;
+  static const double omegaEarth = 7292115.1467e-11;
+  static const double gmWGS      = 398.6005e12;
+
+  memset(xc, 0, 4*sizeof(double));
+  memset(vv, 0, 3*sizeof(double));
+
+  double a0 = _sqrt_A * _sqrt_A;
+  if (a0 == 0) {
+    return;
+  }
+
+  double n0 = sqrt(gmWGS/(a0*a0*a0));
+  double tk = GPSweeks - _TOE;
+  if (GPSweek != _GPSweek) {  
+    tk += (GPSweek - _GPSweek) * secPerWeek;
+  }
+  double n  = n0 + _Delta_n;
+  double M  = _M0 + n*tk;
+  double E  = M;
+  double E_last;
+  do {
+    E_last = E;
+    E = M + _e*sin(E);
+  } while ( fabs(E-E_last)*a0 > 0.001 );
+  double v      = 2.0*atan( sqrt( (1.0 + _e)/(1.0 - _e) )*tan( E/2 ) );
+  double u0     = v + _omega;
+  double sin2u0 = sin(2*u0);
+  double cos2u0 = cos(2*u0);
+  double r      = a0*(1 - _e*cos(E)) + _Crc*cos2u0 + _Crs*sin2u0;
+  double i      = _i0 + _IDOT*tk + _Cic*cos2u0 + _Cis*sin2u0;
+  double u      = u0 + _Cuc*cos2u0 + _Cus*sin2u0;
+  double xp     = r*cos(u);
+  double yp     = r*sin(u);
+  double OM     = _OMEGA0 + (_OMEGADOT - omegaEarth)*tk - 
+                   omegaEarth*_TOE;
+  
+  double sinom = sin(OM);
+  double cosom = cos(OM);
+  double sini  = sin(i);
+  double cosi  = cos(i);
+  xc[0] = xp*cosom - yp*cosi*sinom;
+  xc[1] = xp*sinom + yp*cosi*cosom;
+  xc[2] = yp*sini;                 
+  
+  double tc = GPSweeks - _TOC;
+  if (GPSweek != _GPSweek) {  
+    tc += (GPSweek - _GPSweek) * secPerWeek;
+  }
+  xc[3] = _clock_bias + _clock_drift*tc + _clock_driftrate*tc*tc;
+
+  // Velocity
+  // --------
+  double tanv2 = tan(v/2);
+  double dEdM  = 1 / (1 - _e*cos(E));
+  double dotv  = sqrt((1.0 + _e)/(1.0 - _e)) / cos(E/2)/cos(E/2) / (1 + tanv2*tanv2) 
+               * dEdM * n;
+  double dotu  = dotv + (-_Cuc*sin2u0 + _Cus*cos2u0)*2*dotv;
+  double dotom = _OMEGADOT - omegaEarth;
+  double doti  = _IDOT + (-_Cic*sin2u0 + _Cis*cos2u0)*2*dotv;
+  double dotr  = a0 * _e*sin(E) * dEdM * n 
+                + (-_Crc*sin2u0 + _Crs*cos2u0)*2*dotv;
+  double dotx  = dotr*cos(u) - r*sin(u)*dotu;
+  double doty  = dotr*sin(u) + r*cos(u)*dotu;
+
+  vv[0]  = cosom   *dotx  - cosi*sinom   *doty      // dX / dr
+           - xp*sinom*dotom - yp*cosi*cosom*dotom   // dX / dOMEGA
+                       + yp*sini*sinom*doti;        // dX / di
+
+  vv[1]  = sinom   *dotx  + cosi*cosom   *doty
+           + xp*cosom*dotom - yp*cosi*sinom*dotom
+                          - yp*sini*cosom*doti;
+
+  vv[2]  = sini    *doty  + yp*cosi      *doti;
+
+  // Relativistic Correction
+  // -----------------------
+  //  xc(4) -= 4.442807633e-10 * _e * sqrt(a0) *sin(E);
+  xc[3] -= 2.0 * (xc[0]*vv[0] + xc[1]*vv[1] + xc[2]*vv[2]) / t_CST::c / t_CST::c;
+}
+