#include <sstream>
#include <iostream>
#include <iomanip>
#include <cstring>

#include <newmatio.h>

#include "ephemeris.h"
#include "bncutils.h"
#include "bnctime.h"
#include "bnccore.h"
#include "bncutils.h"
#include "satObs.h"
#include "pppInclude.h"
#include "pppModel.h"
#include "RTCM3/bits.h"

using namespace std;

// Constructor
////////////////////////////////////////////////////////////////////////////
t_eph::t_eph() {
  _checkState = unchecked;
  _navType = undefined;
  _orbCorr    = 0;
  _clkCorr    = 0;
}
// Destructor
////////////////////////////////////////////////////////////////////////////
t_eph::~t_eph() {
  if (_orbCorr)
    delete _orbCorr;
  if (_clkCorr)
    delete _clkCorr;
}

//
////////////////////////////////////////////////////////////////////////////
void t_eph::setOrbCorr(const t_orbCorr* orbCorr) {
  if (_orbCorr) {
    delete _orbCorr;
    _orbCorr = 0;
  }
  _orbCorr = new t_orbCorr(*orbCorr);
}

//
////////////////////////////////////////////////////////////////////////////
void t_eph::setClkCorr(const t_clkCorr* clkCorr) {
  if (_clkCorr) {
    delete _clkCorr;
    _clkCorr = 0;
  }
  _clkCorr = new t_clkCorr(*clkCorr);
}

//
////////////////////////////////////////////////////////////////////////////
t_irc t_eph::getCrd(const bncTime& tt, ColumnVector& xc, ColumnVector& vv, bool useCorr) const {

  if (_checkState == bad ||
      _checkState == unhealthy ||
      _checkState == outdated) {
    return failure;
  }

  xc.ReSize(6);
  vv.ReSize(3);
  if (position(tt.gpsw(), tt.gpssec(), xc.data(), vv.data()) != success) {
    return failure;
  }
  if (useCorr) {
    if (_orbCorr && _clkCorr) {
      double dtO = tt - _orbCorr->_time;
      if (_orbCorr->_updateInt) {
        dtO -= (0.5 * ssrUpdateInt[_orbCorr->_updateInt]);
      }
      ColumnVector dx(3);
      dx[0] = _orbCorr->_xr[0] + _orbCorr->_dotXr[0] * dtO;
      dx[1] = _orbCorr->_xr[1] + _orbCorr->_dotXr[1] * dtO;
      dx[2] = _orbCorr->_xr[2] + _orbCorr->_dotXr[2] * dtO;

      RSW_to_XYZ(xc.Rows(1,3), vv.Rows(1,3), dx, dx);

      xc[0] -= dx[0];
      xc[1] -= dx[1];
      xc[2] -= dx[2];

      ColumnVector dv(3);
      RSW_to_XYZ(xc.Rows(1,3), vv.Rows(1,3), _orbCorr->_dotXr, dv);

      vv[0] -= dv[0];
      vv[1] -= dv[1];
      vv[2] -= dv[2];

      double dtC = tt - _clkCorr->_time;
      if (_clkCorr->_updateInt) {
        dtC -= (0.5 * ssrUpdateInt[_clkCorr->_updateInt]);
      }
      xc[3] += _clkCorr->_dClk + _clkCorr->_dotDClk * dtC + _clkCorr->_dotDotDClk * dtC * dtC;
    }
    else {
      return failure;
    }
  }
  return success;
}


//
//////////////////////////////////////////////////////////////////////////////
t_irc t_eph::setNavType(QString navTypeStr) {
  if      (navTypeStr == "LNAV") {
    _navType =  t_eph::LNAV;
  }
  else if (navTypeStr == "FDMA") {
    _navType =  t_eph::FDMA;
  }
  else if (navTypeStr == "FNAV") {
    _navType =  t_eph::FNAV;
  }
  else if (navTypeStr == "INAV") {
    _navType =  t_eph::INAF;
  }
  else if (navTypeStr == "D1")   {
    _navType =  t_eph::D1;
  }
  else if (navTypeStr == "D2")   {
    _navType =  t_eph::D2;
  }
  else if (navTypeStr == "SBAS") {
    _navType =  t_eph::SBASL1;
  }
  else if (navTypeStr == "CNAV") {
    _navType =  t_eph::CNAV;
  }
  else if (navTypeStr == "CNV1") {
    _navType =  t_eph::CNV1;
  }
  else if (navTypeStr == "CNV2") {
    _navType =  t_eph::CNV2;
  }
  else if (navTypeStr == "CNV3") {
    _navType =  t_eph::CNV3;
  }
  else                           {
    _navType = t_eph::undefined;
    return failure;
  }

  return success;
}

//
//////////////////////////////////////////////////////////////////////////////
QString t_eph::navTypeString(e_navType navType, const t_prn& prn, double version) {
    QString navTypeString = "";
    QString epochStart;
    QString eolStr;

    if (version < 4.0) {
      return navTypeString;
    }

    if (version == 99.0) {
      epochStart = "";
      eolStr = "";
    }
    else {
      epochStart = "> ";
      eolStr = "\n";
    }

    QString ephStr = QString("EPH %1 ").arg(prn.toString().c_str());
    switch (navType) {
      case undefined:
        navTypeString = epochStart + ephStr + "unknown" + eolStr;
        break;
      case LNAV:
        navTypeString = epochStart + ephStr + "LNAV" + eolStr;
        break;
      case FDMA:
        navTypeString = epochStart + ephStr + "FDMA" + eolStr;
        break;
      case FNAV:
        navTypeString = epochStart + ephStr + "FNAV" + eolStr;
        break;
      case INAF:
        navTypeString = epochStart + ephStr + "INAV" + eolStr;
        break;
      case D1:
        navTypeString = epochStart + ephStr + "D1  " + eolStr;
        break;
      case D2:
        navTypeString = epochStart + ephStr + "D2  " + eolStr;
        break;
      case SBASL1:
        navTypeString = epochStart + ephStr + "SBAS" + eolStr;
        break;
      case CNAV:
        navTypeString = epochStart + ephStr + "CNAV" + eolStr;
        break;
      case CNV1:
        navTypeString = epochStart + ephStr + "CNV1" + eolStr;
        break;
      case CNV2:
        navTypeString = epochStart + ephStr + "CNV2" + eolStr;
        break;
      case CNV3:
        navTypeString = epochStart + ephStr + "CNV3" + eolStr;
        break;
    }
    return navTypeString;
  }

//
//////////////////////////////////////////////////////////////////////////////
QString t_eph::rinexDateStr(const bncTime& tt, const t_prn& prn, double version) {
  QString prnStr(prn.toString().c_str());
  return rinexDateStr(tt, prnStr, version);
}

//
//////////////////////////////////////////////////////////////////////////////
QString t_eph::rinexDateStr(const bncTime& tt, const QString& prnStr, double version) {

  QString datStr;

  unsigned year, month, day, hour, min;
  double   sec;
  tt.civil_date(year, month, day);
  tt.civil_time(hour, min, sec);

  QTextStream out(&datStr);

  if (version < 3.0) {
    QString prnHlp = prnStr.mid(1,2); if (prnHlp[0] == '0') prnHlp[0] = ' ';
    out << prnHlp << QString(" %1 %2 %3 %4 %5%6")
      .arg(year % 100, 2, 10, QChar('0'))
      .arg(month,      2)
      .arg(day,        2)
      .arg(hour,       2)
      .arg(min,        2)
      .arg(sec, 5, 'f',1);
  }
  else if (version ==  99) {
    out << QString(" %1 %2 %3 %4 %5 %6")
      .arg(year,     4)
      .arg(month,    2, 10, QChar('0'))
      .arg(day,      2, 10, QChar('0'))
      .arg(hour,     2, 10, QChar('0'))
      .arg(min,      2, 10, QChar('0'))
      .arg(int(sec), 2, 10, QChar('0'));
  }
  else {
    out << prnStr << QString(" %1 %2 %3 %4 %5 %6")
      .arg(year,     4)
      .arg(month,    2, 10, QChar('0'))
      .arg(day,      2, 10, QChar('0'))
      .arg(hour,     2, 10, QChar('0'))
      .arg(min,      2, 10, QChar('0'))
      .arg(int(sec), 2, 10, QChar('0'));
  }

  return datStr;
}

// Constructor
//////////////////////////////////////////////////////////////////////////////
t_ephGPS::t_ephGPS(double rnxVersion, const QStringList& lines) {

  int nLines = 8;

  if (navType() == t_eph::CNAV) {
    nLines += 1;
  }
  if (navType() == t_eph::CNV2) {
    nLines += 2;
  }

  if (lines.size() != nLines) {
    _checkState = bad;
    return;
  }

  // RINEX Format
  // ------------
  int fieldLen = 19;

  int pos[4];
  pos[0] = (rnxVersion <= 2.12) ?  3 :  4;
  pos[1] = pos[0] + fieldLen;
  pos[2] = pos[1] + fieldLen;
  pos[3] = pos[2] + fieldLen;

  // Read eight lines
  // ----------------
  for (int iLine = 0; iLine < nLines; iLine++) {
    QString line = lines[iLine];

    if      ( iLine == 0 ) {
      QTextStream in(line.left(pos[1]).toLatin1());
      int    year, month, day, hour, min;
      double sec;

      QString prnStr, n;
      in >> prnStr;

      if (prnStr.size() == 1 &&
          (prnStr[0] == 'G' ||
           prnStr[0] == 'J' ||
           prnStr[0] == 'I')) {
        in >> n;
        prnStr.append(n);
      }

      in >> year >> month >> day >> hour >> min >> sec;
      if      (prnStr.at(0) == 'G') {
        _prn.set('G', prnStr.mid(1).toInt());
      }
      else if (prnStr.at(0) == 'J') {
        _prn.set('J', prnStr.mid(1).toInt());
      }
      else if (prnStr.at(0) == 'I') {
        _prn.set('I', prnStr.mid(1).toInt());
      }
      else {
        _prn.set('G', prnStr.toInt());
      }

      if      (year <  80) {
        year += 2000;
      }
      else if (year < 100) {
        year += 1900;
      }

      _TOC.set(year, month, day, hour, min, sec);

    if   ( readDbl(line, pos[1], fieldLen, _clock_bias     ) ||
           readDbl(line, pos[2], fieldLen, _clock_drift    ) ||
           readDbl(line, pos[3], fieldLen, _clock_driftrate) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 1
    // =====================
    else if      ( iLine == 1) {

      if (navType() == t_eph::CNAV ||
          navType() == t_eph::CNV2) {
        if ( readDbl(line, pos[0], fieldLen, _ADOT   ) ||
             readDbl(line, pos[1], fieldLen, _Crs    ) ||
             readDbl(line, pos[2], fieldLen, _Delta_n) ||
             readDbl(line, pos[3], fieldLen, _M0     ) ) {
              _checkState = bad;
                return;
                }
      }
      else { // LNAV, undefined
        if ( readDbl(line, pos[0], fieldLen, _IODE   ) ||
             readDbl(line, pos[1], fieldLen, _Crs    ) ||
             readDbl(line, pos[2], fieldLen, _Delta_n) ||
             readDbl(line, pos[3], fieldLen, _M0     ) ) {
          _checkState = bad;
          return;
        }
      }
    }
    // =====================
    // BROADCAST ORBIT - 2
    // =====================
    else if ( iLine == 2 ) {
      if ( readDbl(line, pos[0], fieldLen, _Cuc   ) ||
           readDbl(line, pos[1], fieldLen, _e     ) ||
           readDbl(line, pos[2], fieldLen, _Cus   ) ||
           readDbl(line, pos[3], fieldLen, _sqrt_A) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 3
    // =====================
    else if ( iLine == 3 ) {

      if (navType() == t_eph::CNAV ||
          navType() == t_eph::CNV2) {
        if ( readDbl(line, pos[0], fieldLen, _top)  ||
             readDbl(line, pos[1], fieldLen, _Cic   )  ||
             readDbl(line, pos[2], fieldLen, _OMEGA0)  ||
             readDbl(line, pos[3], fieldLen, _Cis   ) ) {
          _checkState = bad;
          return;
        }
      }
      else { // LNAV, undefined
        if ( readDbl(line, pos[0], fieldLen, _TOEsec)  ||
             readDbl(line, pos[1], fieldLen, _Cic   )  ||
             readDbl(line, pos[2], fieldLen, _OMEGA0)  ||
             readDbl(line, pos[3], fieldLen, _Cis   ) ) {
          _checkState = bad;
          return;
        }
      }
    }
    // =====================
    // BROADCAST ORBIT - 4
    // =====================
    else if ( iLine == 4 ) {
      if ( readDbl(line, pos[0], fieldLen, _i0      ) ||
           readDbl(line, pos[1], fieldLen, _Crc     ) ||
           readDbl(line, pos[2], fieldLen, _omega   ) ||
           readDbl(line, pos[3], fieldLen, _OMEGADOT) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 5
    // =====================
    else if ( iLine == 5 && type() != t_eph::IRNSS) {

      if (navType() == t_eph::CNAV ||
          navType() == t_eph::CNV2) {
        if ( readDbl(line, pos[0], fieldLen, _IDOT       ) ||
             readDbl(line, pos[1], fieldLen, _Delta_n_dot) ||
             readDbl(line, pos[2], fieldLen, _URAI_NED0  ) ||
             readDbl(line, pos[3], fieldLen, _URAI_NED1) ) {
          _checkState = bad;
          return;
        }
      }
      else { // LNAV, undefined
        if ( readDbl(line, pos[0], fieldLen, _IDOT   ) ||
             readDbl(line, pos[1], fieldLen, _L2Codes) ||
             readDbl(line, pos[2], fieldLen, _TOEweek) ||
             readDbl(line, pos[3], fieldLen, _L2PFlag) ) {
          _checkState = bad;
          return;
        }
      }
    }
    else if ( iLine == 5 && type() == t_eph::IRNSS) {
      if ( readDbl(line, pos[0], fieldLen, _IDOT   ) ||
           readDbl(line, pos[2], fieldLen, _TOEweek) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 6
    // =====================
    else if ( iLine == 6 && type() != t_eph::IRNSS) {

      if (navType() == t_eph::CNAV ||
          navType() == t_eph::CNV2  ) {
        if ( readDbl(line, pos[0], fieldLen, _URAI_ED) ||
             readDbl(line, pos[1], fieldLen, _health ) ||
             readDbl(line, pos[2], fieldLen, _TGD    ) ||
             readDbl(line, pos[3], fieldLen, _URAI_NED2) ) {
          _checkState = bad;
          return;
        }
      }
      else { // LNAV, undefined
        if ( readDbl(line, pos[0], fieldLen, _ura   ) ||
             readDbl(line, pos[1], fieldLen, _health) ||
             readDbl(line, pos[2], fieldLen, _TGD   ) ||
             readDbl(line, pos[3], fieldLen, _IODC  ) ) {
          _checkState = bad;
          return;
        }
      }
    }
    else if ( iLine == 6 && type() == t_eph::IRNSS) {
      if ( readDbl(line, pos[0], fieldLen, _ura   ) ||
           readDbl(line, pos[1], fieldLen, _health) ||
           readDbl(line, pos[2], fieldLen, _TGD   ) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 7
    // =====================
    else if ( iLine == 7 ) {
      if (navType() == t_eph::LNAV ||
          navType() == t_eph::undefined) {

        if ( readDbl(line, pos[0], fieldLen, _TOT) ) {
          _checkState = bad;
          return;
        }

        if (type() != t_eph::IRNSS) {
          double fitIntervalRnx;
          if ( readDbl(line, pos[1], fieldLen, fitIntervalRnx) ) {
            _checkState = bad;
            return;
          }
          if        (type() == t_eph::GPS) {  // in RINEX specified always as time period for GPS
              _fitInterval = fitIntervalRnx;
          } else if (type() == t_eph::QZSS) { // specified as flag for QZSS
            if (rnxVersion == 3.02) {
              _fitInterval = fitIntervalRnx; // specified as time period
            }
            else {
              _fitInterval = fitIntervalFromFlag(fitIntervalRnx, _IODC, t_eph::QZSS);
            }
          }
        }
      }

      else if (navType() == t_eph::CNAV ||
               navType() == t_eph::CNV2) {
        if ( readDbl(line, pos[0], fieldLen, _ISC_L1CA) ||
             readDbl(line, pos[1], fieldLen, _ISC_L2C ) ||
             readDbl(line, pos[2], fieldLen, _ISC_L5I5) ||
             readDbl(line, pos[3], fieldLen, _ISC_L5Q5) ) {
          _checkState = bad;
          return;
        }
      }

    }
    // =====================
    // BROADCAST ORBIT - 8
    // =====================
    else if ( iLine == 8 ) {
      if (navType() == t_eph::CNAV) {
        if ( readDbl(line, pos[0], fieldLen, _TOT) ||
             readDbl(line, pos[1], fieldLen, _wnop) ) {
          _checkState = bad;
          return;
        }
      }
      else if (navType() == t_eph::CNV2) {
        if ( readDbl(line, pos[0], fieldLen, _ISC_L1Cd) ||
             readDbl(line, pos[1], fieldLen, _ISC_L1Cp)) {
          _checkState = bad;
          return;
        }
      }
    }
    // =====================
    // BROADCAST ORBIT - 9
    // =====================
    else if ( iLine == 9 ) {
      if (navType() == t_eph::CNV2) {
        if ( readDbl(line, pos[0], fieldLen, _TOT) ||
             readDbl(line, pos[1], fieldLen, _wnop) ) {
          _checkState = bad;
          return;
        }
      }
    }
  }
}

// Compute GPS Satellite Position (virtual)
////////////////////////////////////////////////////////////////////////////
t_irc t_ephGPS::position(int GPSweek, double GPSweeks, double* xc, double* vv) const {

  static const double omegaEarth = 7292115.1467e-11;
  static const double gmGRS      = 398.6005e12;

  memset(xc, 0, 6*sizeof(double));
  memset(vv, 0, 3*sizeof(double));

  double a0 = _sqrt_A * _sqrt_A;
  if (a0 == 0) {
    return failure;
  }

  double n0 = sqrt(gmGRS/(a0*a0*a0));

  bncTime tt(GPSweek, GPSweeks);
  double tk = tt - bncTime(int(_TOEweek), _TOEsec);

  double n  = n0 + _Delta_n;
  double M  = _M0 + n*tk;
  double E  = M;
  double E_last;
  int    nLoop = 0;
  do {
    E_last = E;
    E = M + _e*sin(E);

    if (++nLoop == 100) {
      return failure;
    }
  } 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*_TOEsec;

  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 = tt - _TOC;
  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[3] -= 4.442807633e-10 * _e * sqrt(a0) *sin(E);

  xc[4] = _clock_drift + _clock_driftrate*tc;
  xc[5] = _clock_driftrate;

  return success;
}

// RINEX Format String
//////////////////////////////////////////////////////////////////////////////
QString t_ephGPS::toString(double version) const {

  QString navStr = navTypeString(_navType, _prn, version);
  QString rnxStr = navStr + rinexDateStr(_TOC, _prn, version);

  QTextStream out(&rnxStr);

  out << QString("%1%2%3\n")
    .arg(_clock_bias,      19, 'e', 12)
    .arg(_clock_drift,     19, 'e', 12)
    .arg(_clock_driftrate, 19, 'e', 12);

  QString fmt = version < 3.0 ? "   %1%2%3%4\n" : "    %1%2%3%4\n";


  // =====================
  // BROADCAST ORBIT - 1
  // =====================
  if (navType() == t_eph::CNAV ||
      navType() == t_eph::CNV2) {
    out << QString(fmt)
      .arg(_ADOT,    19, 'e', 12)
      .arg(_Crs,     19, 'e', 12)
      .arg(_Delta_n, 19, 'e', 12)
      .arg(_M0,      19, 'e', 12);
  }
  else { // LNAV, undefinded
    out << QString(fmt)
      .arg(_IODE,    19, 'e', 12)
      .arg(_Crs,     19, 'e', 12)
      .arg(_Delta_n, 19, 'e', 12)
      .arg(_M0,      19, 'e', 12);
  }
  // =====================
  // BROADCAST ORBIT - 2
  // =====================
  out << QString(fmt)
    .arg(_Cuc,    19, 'e', 12)
    .arg(_e,      19, 'e', 12)
    .arg(_Cus,    19, 'e', 12)
    .arg(_sqrt_A, 19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 3
  // =====================
  if (navType() == t_eph::CNAV ||
      navType() == t_eph::CNV2) {
    out << QString(fmt)
        .arg(_top,    19, 'e', 12)
        .arg(_Cic,    19, 'e', 12)
        .arg(_OMEGA0, 19, 'e', 12)
        .arg(_Cis,    19, 'e', 12);
  }
  else {
    out << QString(fmt)
        .arg(_TOEsec, 19, 'e', 12)
        .arg(_Cic,    19, 'e', 12)
        .arg(_OMEGA0, 19, 'e', 12)
        .arg(_Cis,    19, 'e', 12);
  }
  // =====================
  // BROADCAST ORBIT - 4
  // =====================
  out << QString(fmt)
    .arg(_i0,       19, 'e', 12)
    .arg(_Crc,      19, 'e', 12)
    .arg(_omega,    19, 'e', 12)
    .arg(_OMEGADOT, 19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 5
  // =====================
  if (type() == t_eph::IRNSS) {
    out << QString(fmt)
      .arg(_IDOT,    19, 'e', 12)
      .arg(0.0,      19, 'e', 12)
      .arg(_TOEweek, 19, 'e', 12)
      .arg(0.0,      19, 'e', 12);
  }
  else {
    if (navType() == t_eph::CNAV ||
        navType() == t_eph::CNV2) {
      out << QString(fmt)
        .arg(_IDOT,        19, 'e', 12)
        .arg(_Delta_n_dot, 19, 'e', 12)
        .arg(_URAI_NED0,   19, 'e', 12)
        .arg(_URAI_NED1,   19, 'e', 12);

    }
    else { // LNAV, undefined
      out << QString(fmt)
        .arg(_IDOT,    19, 'e', 12)
        .arg(_L2Codes, 19, 'e', 12)
        .arg(_TOEweek, 19, 'e', 12)
        .arg(_L2PFlag, 19, 'e', 12);

    }
  }
  // =====================
  // BROADCAST ORBIT - 6
  // =====================
  if (type() == t_eph::IRNSS) {
    out << QString(fmt)
      .arg(_ura,    19, 'e', 12)
      .arg(_health, 19, 'e', 12)
      .arg(_TGD,    19, 'e', 12)
      .arg(0.0,     19, 'e', 12);
  }
  else {
    if (navType() == t_eph::CNAV ||
        navType() == t_eph::CNV2) {
      out << QString(fmt)
        .arg(_URAI_ED,  19, 'e', 12)
        .arg(_health,   19, 'e', 12)
        .arg(_TGD,      19, 'e', 12)
        .arg(_URAI_NED2,19, 'e', 12);

    }
    else { // LNAV, undefined
      out << QString(fmt)
        .arg(_ura,    19, 'e', 12)
        .arg(_health, 19, 'e', 12)
        .arg(_TGD,    19, 'e', 12)
        .arg(_IODC,   19, 'e', 12);
    }
  }
  // =====================
  // BROADCAST ORBIT - 7
  // =====================
  if (navType() == t_eph::LNAV ||
      navType() == t_eph::undefined) {

    double tot = _TOT;
    if (tot == 0.9999e9 && version < 3.0) {
      tot = 0.0;
    }
    // fitInterval
    if (type() == t_eph::IRNSS) {// not valid for IRNSS
      out << QString(fmt)
        .arg(tot,          19, 'e', 12)
        .arg(0.0,          19, 'e', 12)
        .arg("",           19, QChar(' '))
        .arg("",           19, QChar(' '));
    }
    else {
      // for GPS and QZSS in version 3.02 specified in hours
      double fitIntervalRnx = _fitInterval;
      // otherwise specified as flag
      if (type() == t_eph::QZSS && version != 3.02) {
        (_fitInterval == 2.0) ? fitIntervalRnx = 0.0 : fitIntervalRnx = 1.0;
      }
      out << QString(fmt)
        .arg(tot,            19, 'e', 12)
        .arg(fitIntervalRnx, 19, 'e', 12)
        .arg("",             19, QChar(' '))
        .arg("",             19, QChar(' '));
    }
  }
  else if (navType() == t_eph::CNAV ||
           navType() == t_eph::CNV2) {
    out << QString(fmt)
      .arg(_ISC_L1CA, 19, 'e', 12)
      .arg(_ISC_L2C,  19, 'e', 12)
      .arg(_ISC_L5I5, 19, 'e', 12)
      .arg(_ISC_L5Q5, 19, 'e', 12);
  }
  // =====================
  // BROADCAST ORBIT - 8
  // =====================
  if (navType() == t_eph::CNAV) {
    out << QString(fmt)
      .arg(_TOT,  19, 'e', 12)
      .arg(_wnop, 19, 'e', 12)
      .arg("",    19, QChar(' '))
      .arg("",    19, QChar(' '));
  }
  else if (navType() == t_eph::CNV2) {
    out << QString(fmt)
      .arg(_ISC_L1Cd, 19, 'e', 12)
      .arg(_ISC_L1Cp, 19, 'e', 12)
      .arg("",        19, QChar(' '))
      .arg("",        19, QChar(' '));
  }

  // =====================
  // BROADCAST ORBIT - 9
  // =====================
  if (navType() == t_eph::CNV2) {
    out << QString(fmt)
      .arg(_TOT,  19, 'e', 12)
      .arg(_wnop, 19, 'e', 12)
      .arg("",    19, QChar(' '))
      .arg("",    19, QChar(' '));
  }

  return rnxStr;
}

// Constructor
//////////////////////////////////////////////////////////////////////////////
t_ephGlo::t_ephGlo(double rnxVersion, const QStringList& lines) {

  int nLines = 4;
  if (rnxVersion >= 3.05) {
    nLines += 1;
  }
  else {
    _M_delta_tau = 0.9999e9; // unknown
    _M_FT = 1.5e1;           // unknown
  }

  if (lines.size() != nLines) {
    _checkState = bad;
    return;
  }

  // RINEX Format
  // ------------
  int fieldLen = 19;
  double statusflags = 0.0;
  double healthflags = 0.0;

  int pos[4];
  pos[0] = (rnxVersion <= 2.12) ?  3 :  4;
  pos[1] = pos[0] + fieldLen;
  pos[2] = pos[1] + fieldLen;
  pos[3] = pos[2] + fieldLen;

  // Read four lines
  // ---------------
  for (int iLine = 0; iLine < nLines; iLine++) {
    QString line = lines[iLine];

    if      ( iLine == 0 ) {
      QTextStream in(line.left(pos[1]).toLatin1());

      int    year, month, day, hour, min;
      double sec;

      QString prnStr, n;
      in >> prnStr;
      if (prnStr.size() == 1 && prnStr[0] == 'R') {
        in >> n;
        prnStr.append(n);
      }
      in >> year >> month >> day >> hour >> min >> sec;
      if (prnStr.at(0) == 'R') {
        _prn.set('R', prnStr.mid(1).toInt());
      }
      else {
        _prn.set('R', prnStr.toInt());
      }

      if      (year <  80) {
        year += 2000;
      }
      else if (year < 100) {
        year += 1900;
      }

      _gps_utc = gnumleap(year, month, day);

      _TOC.set(year, month, day, hour, min, sec);
      _TOC  = _TOC + _gps_utc;
      int nd = int((_TOC.gpssec())) / (24.0*60.0*60.0);
      if ( readDbl(line, pos[1], fieldLen, _tau  ) ||
           readDbl(line, pos[2], fieldLen, _gamma) ||
           readDbl(line, pos[3], fieldLen, _tki  ) ) {
        _checkState = bad;
        return;
      }
      _tki -= nd * 86400.0;
      _tau  = -_tau;
    }
    // =====================
    // BROADCAST ORBIT - 1
    // =====================
    else if      ( iLine == 1 ) {
      if ( readDbl(line, pos[0], fieldLen, _x_pos         ) ||
           readDbl(line, pos[1], fieldLen, _x_velocity    ) ||
           readDbl(line, pos[2], fieldLen, _x_acceleration) ||
           readDbl(line, pos[3], fieldLen, _health        ) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 2
    // =====================
    else if ( iLine == 2 ) {
      if ( readDbl(line, pos[0], fieldLen, _y_pos           ) ||
           readDbl(line, pos[1], fieldLen, _y_velocity      ) ||
           readDbl(line, pos[2], fieldLen, _y_acceleration  ) ||
           readDbl(line, pos[3], fieldLen, _frequency_number) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 3
    // =====================
    else if ( iLine == 3 ) {
      if ( readDbl(line, pos[0], fieldLen, _z_pos         )  ||
           readDbl(line, pos[1], fieldLen, _z_velocity    )  ||
           readDbl(line, pos[2], fieldLen, _z_acceleration)  ||
           readDbl(line, pos[3], fieldLen, _E             ) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 4
    // =====================
    else if ( iLine == 4 ) {
      if (readDbl(line, pos[0], fieldLen, statusflags    ) ) {
        //statusflags BLK, do nothing
        _flags_unknown = true;
      }
      else {
        _flags_unknown = false;
        // status flags
        // ============
        // bit 0-1
        _M_P  = double(bitExtracted(statusflags, 2, 0));
        // bit 2-3
        _P1   = double(bitExtracted(statusflags, 2, 2));
        // bit 4
        _P2   = double(bitExtracted(statusflags, 1, 4));
        // bit 5
        _P3   = double(bitExtracted(statusflags, 1, 5));
        // bit 6
        _M_P4 = double(bitExtracted(statusflags, 1, 6));
        // bit 7-8
        _M_M  = double(bitExtracted(statusflags, 2, 7));
        /// GLO M/K exclusive flags/values only valid if flag M is set to '01'
        if (!_M_M) {
          _M_P4 = 0.0;
          _M_P  = 0.0;
        }
      }
      if ( readDbl(line, pos[1], fieldLen, _M_delta_tau   )  ||
           readDbl(line, pos[2], fieldLen, _M_FT          ) ) {
        _checkState = bad;
        return;
      }
      if (readDbl(line, pos[3], fieldLen, healthflags    ) ) {
        // healthflags BLK
        _flags_unknown = true;
      }
      else {
        _flags_unknown = false;
        // health flags
        // ============
        // bit 0 (is to be ignored, if bit 1 is zero)
        _almanac_health = double(bitExtracted(healthflags, 1, 0));
        // bit 1
        _almanac_health_availablility_indicator = double(bitExtracted(healthflags, 1, 1));
        //  bit 2
        _M_l3 = double(bitExtracted(healthflags, 1, 2));
      }
    }
  }

  // Initialize status vector
  // ------------------------
  _tt = _TOC;
  _xv.ReSize(6); _xv = 0.0;
  _xv(1) = _x_pos * 1.e3;
  _xv(2) = _y_pos * 1.e3;
  _xv(3) = _z_pos * 1.e3;
  _xv(4) = _x_velocity * 1.e3;
  _xv(5) = _y_velocity * 1.e3;
  _xv(6) = _z_velocity * 1.e3;
}

// Compute Glonass Satellite Position (virtual)
////////////////////////////////////////////////////////////////////////////
t_irc t_ephGlo::position(int GPSweek, double GPSweeks, double* xc, double* vv) const {

  static const double nominalStep = 10.0;

  memset(xc, 0, 6*sizeof(double));
  memset(vv, 0, 3*sizeof(double));

  double dtPos = bncTime(GPSweek, GPSweeks) - _tt;

  if (fabs(dtPos) > 24 * 3600.0) {
    return failure;
  }

  int nSteps  = int(fabs(dtPos) / nominalStep) + 1;
  double step = dtPos / nSteps;

  double acc[3];
  acc[0] = _x_acceleration * 1.e3;
  acc[1] = _y_acceleration * 1.e3;
  acc[2] = _z_acceleration * 1.e3;

  for (int ii = 1; ii <= nSteps; ii++) {
    _xv = rungeKutta4(_tt.gpssec(), _xv, step, acc, glo_deriv);
    _tt = _tt + step;
  }

  // Position and Velocity
  // ---------------------
  xc[0] = _xv(1);
  xc[1] = _xv(2);
  xc[2] = _xv(3);

  vv[0] = _xv(4);
  vv[1] = _xv(5);
  vv[2] = _xv(6);

  // Clock Correction
  // ----------------
  double dtClk = bncTime(GPSweek, GPSweeks) - _TOC;
  xc[3] = -_tau + _gamma * dtClk;

  xc[4] = _gamma;
  xc[5] = 0.0;

  return success;
}

// RINEX Format String
//////////////////////////////////////////////////////////////////////////////
QString t_ephGlo::toString(double version) const {

  QString navStr = navTypeString(_navType, _prn, version);
  QString rnxStr = navStr + rinexDateStr(_TOC -_gps_utc, _prn, version);
  int nd = int((_TOC - _gps_utc).gpssec()) / (24.0*60.0*60.0);
  QTextStream out(&rnxStr);

  out << QString("%1%2%3\n")
    .arg(-_tau,           19, 'e', 12)
    .arg(_gamma,          19, 'e', 12)
    .arg(_tki+nd*86400.0, 19, 'e', 12);

  QString fmt = version < 3.0 ? "   %1%2%3%4\n" : "    %1%2%3%4\n";
  // =====================
  // BROADCAST ORBIT - 1
  // =====================
  out << QString(fmt)
    .arg(_x_pos,          19, 'e', 12)
    .arg(_x_velocity,     19, 'e', 12)
    .arg(_x_acceleration, 19, 'e', 12)
    .arg(_health,         19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 2
  // =====================
  out << QString(fmt)
    .arg(_y_pos,            19, 'e', 12)
    .arg(_y_velocity,       19, 'e', 12)
    .arg(_y_acceleration,   19, 'e', 12)
    .arg(_frequency_number, 19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 3
  // =====================
  out << QString(fmt)
    .arg(_z_pos,          19, 'e', 12)
    .arg(_z_velocity,     19, 'e', 12)
    .arg(_z_acceleration, 19, 'e', 12)
    .arg(_E,              19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 4
  // =====================
  if (version >= 3.05) {
    // unknown (RINEX version < 3.05)
    if (_flags_unknown) {
      out << QString(fmt)
        .arg("",            19, QChar(' '))  // statusflags blank if unknown
        .arg(_M_delta_tau,  19, 'e', 12)
        .arg(_M_FT,         19, 'e', 12)
        .arg("",            19, QChar(' ')); // healthflags blank if unknown
    }
    else {
      int statusflags = 0;
      // bit 7-8
      if (_M_M == 2.0) {
        statusflags |= (1<<7);
      }
      // bit 6
      if (_M_P4) {
        statusflags |= (1<<6);
      }
      // bit 5
      if (_P3) {
        statusflags |= (1<<5);
      }
      // bit 4
      if (_P2) {
        statusflags |= (1<<4);
      }
      // bit 2-3
      if      (_P1 == 2.0) {
        statusflags |= (1<<2);
      }
      else if (_P1 == 1.0) {
        statusflags |= (1<<3);
      }
      else if (_P1 == 3.0) {
        statusflags |= (1<<2);
        statusflags |= (1<<3);
      }
      // bit 0-1
      if       (_M_P == 2.0) {
        statusflags |= (1<<0);
      }
      else if (_M_P == 1.0) {
        statusflags |= (1<<1);
      }
      else if (_M_P == 3.0) {
        statusflags |= (1<<0);
        statusflags |= (1<<1);
      }
      // health flags
      // ============
      int healthflags = 0;
      // bit 0 (is to be ignored, if bit 1 is zero)
      if (_almanac_health) {
        healthflags |= (1<<0);
      }
      // bit 1
      if (_almanac_health_availablility_indicator) {
        healthflags |= (1<<1);
      }
      //  bit 2
      if (_M_l3) {
        healthflags |= (1<<2);
      }
      out << QString(fmt)
        .arg(double(statusflags), 19, 'e', 12)
        .arg(_M_delta_tau,        19, 'e', 12)
        .arg(_M_FT,               19, 'e', 12)
        .arg(double(healthflags), 19, 'e', 12);
    }
  }

  return rnxStr;
}

// Derivative of the state vector using a simple force model (static)
////////////////////////////////////////////////////////////////////////////
ColumnVector t_ephGlo::glo_deriv(double /* tt */, const ColumnVector& xv,
                                 double* acc) {

  // State vector components
  // -----------------------
  ColumnVector rr = xv.rows(1,3);
  ColumnVector vv = xv.rows(4,6);

  // Acceleration
  // ------------
  static const double gmWGS = 398.60044e12;
  static const double AE    = 6378136.0;
  static const double OMEGA = 7292115.e-11;
  static const double C20   = -1082.6257e-6;

  double rho = rr.NormFrobenius();
  double t1  = -gmWGS/(rho*rho*rho);
  double t2  = 3.0/2.0 * C20 * (gmWGS*AE*AE) / (rho*rho*rho*rho*rho);
  double t3  = OMEGA * OMEGA;
  double t4  = 2.0 * OMEGA;
  double z2  = rr(3) * rr(3);

  // Vector of derivatives
  // ---------------------
  ColumnVector va(6);
  va(1) = vv(1);
  va(2) = vv(2);
  va(3) = vv(3);
  va(4) = (t1 + t2*(1.0-5.0*z2/(rho*rho)) + t3) * rr(1) + t4*vv(2) + acc[0];
  va(5) = (t1 + t2*(1.0-5.0*z2/(rho*rho)) + t3) * rr(2) - t4*vv(1) + acc[1];
  va(6) = (t1 + t2*(3.0-5.0*z2/(rho*rho))     ) * rr(3)            + acc[2];

  return va;
}

// IOD of Glonass Ephemeris (virtual)
////////////////////////////////////////////////////////////////////////////
unsigned int t_ephGlo::IOD() const {
  bncTime tMoscow = _TOC - _gps_utc + 3 * 3600.0;
  return (unsigned long)tMoscow.daysec() / 900;
}

// Health status of Glonass Ephemeris (virtual)
////////////////////////////////////////////////////////////////////////////
unsigned int t_ephGlo::isUnhealthy() const {

  if (_almanac_health_availablility_indicator) {
      if ((_health == 0 && _almanac_health == 0) ||
          (_health == 1 && _almanac_health == 0) ||
          (_health == 1 && _almanac_health == 1)) {
        return 1;
      }
  }
  else if (!_almanac_health_availablility_indicator) {
    if (_health) {
      return 1;
    }
  }
  return 0; /* (_health == 0 && _almanac_health == 1) or (_health == 0) */
}

// Constructor
//////////////////////////////////////////////////////////////////////////////
t_ephGal::t_ephGal(double rnxVersion, const QStringList& lines) {
  int       year, month, day, hour, min;
  double    sec;
  QString   prnStr;
  const int nLines = 8;
  if (lines.size() != nLines) {
    _checkState = bad;
    return;
  }

  // RINEX Format
  // ------------
  int fieldLen = 19;
  double SVhealth = 0.0;
  double datasource = 0.0;

  int pos[4];
  pos[0] = (rnxVersion <= 2.12) ?  3 :  4;
  pos[1] = pos[0] + fieldLen;
  pos[2] = pos[1] + fieldLen;
  pos[3] = pos[2] + fieldLen;

  // Read eight lines
  // ----------------
  for (int iLine = 0; iLine < nLines; iLine++) {
    QString line = lines[iLine];

    if      ( iLine == 0 ) {
      QTextStream in(line.left(pos[1]).toLatin1());
      QString n;
      in >> prnStr;
      if (prnStr.size() == 1 && prnStr[0] == 'E') {
        in >> n;
        prnStr.append(n);
      }
      in >> year >> month >> day >> hour >> min >> sec;
      if      (year <  80) {
        year += 2000;
      }
      else if (year < 100) {
        year += 1900;
      }

      _TOC.set(year, month, day, hour, min, sec);

      if ( readDbl(line, pos[1], fieldLen, _clock_bias     ) ||
           readDbl(line, pos[2], fieldLen, _clock_drift    ) ||
           readDbl(line, pos[3], fieldLen, _clock_driftrate) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 1
    // =====================
    else if      ( iLine == 1 ) {
      if ( readDbl(line, pos[0], fieldLen, _IODnav ) ||
           readDbl(line, pos[1], fieldLen, _Crs    ) ||
           readDbl(line, pos[2], fieldLen, _Delta_n) ||
           readDbl(line, pos[3], fieldLen, _M0     ) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 2
    // =====================
    else if ( iLine == 2 ) {
      if ( readDbl(line, pos[0], fieldLen, _Cuc   ) ||
           readDbl(line, pos[1], fieldLen, _e     ) ||
           readDbl(line, pos[2], fieldLen, _Cus   ) ||
           readDbl(line, pos[3], fieldLen, _sqrt_A) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 3
    // =====================
    else if ( iLine == 3 ) {
      if ( readDbl(line, pos[0], fieldLen, _TOEsec)  ||
           readDbl(line, pos[1], fieldLen, _Cic   )  ||
           readDbl(line, pos[2], fieldLen, _OMEGA0)  ||
           readDbl(line, pos[3], fieldLen, _Cis   ) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 4
    // =====================
    else if ( iLine == 4 ) {
      if ( readDbl(line, pos[0], fieldLen, _i0      ) ||
           readDbl(line, pos[1], fieldLen, _Crc     ) ||
           readDbl(line, pos[2], fieldLen, _omega   ) ||
           readDbl(line, pos[3], fieldLen, _OMEGADOT) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 5
    // =====================
    else if ( iLine == 5 ) {
      if ( readDbl(line, pos[0], fieldLen, _IDOT      ) ||
           readDbl(line, pos[1], fieldLen, datasource) ||
           readDbl(line, pos[2], fieldLen, _TOEweek   ) ) {
        _checkState = bad;
        return;
      } else {
        if        (int(datasource) & (1<<8)) {
          _fnav = true;
          _inav = false;
        } else if (int(datasource) & (1<<9)) {
          _fnav = false;
          _inav = true;
        }
        _TOEweek -= 1024.0;
      }
    }
    // =====================
    // BROADCAST ORBIT - 6
    // =====================
    else if ( iLine == 6 ) {
      if ( readDbl(line, pos[0], fieldLen, _SISA    ) ||
           readDbl(line, pos[1], fieldLen,  SVhealth) ||
           readDbl(line, pos[2], fieldLen, _BGD_1_5A) ||
           readDbl(line, pos[3], fieldLen, _BGD_1_5B) ) {
        _checkState = bad;
        return;
      } else {
        // Bit 0
        _e1DataInValid  = (int(SVhealth) & (1<<0));
        // Bit 1-2
        _E1_bHS         = double((int(SVhealth) >> 1) & 0x3);
        // Bit 3
        _e5aDataInValid = (int(SVhealth) & (1<<3));
        // Bit 4-5
        _E5aHS          = double((int(SVhealth) >> 4) & 0x3);
        // Bit 6
        _e5bDataInValid = (int(SVhealth) & (1<<6));
        // Bit 7-8
        _E5bHS          = double((int(SVhealth) >> 7) & 0x3);

        if (prnStr.at(0) == 'E') {
          _prn.set('E', prnStr.mid(1).toInt(), _inav ? 1 : 0);
        }
      }
    }
    // =====================
    // BROADCAST ORBIT - 7
    // =====================
    else if ( iLine == 7 ) {
      if ( readDbl(line, pos[0], fieldLen, _TOT) ) {
        _checkState = bad;
        return;
      }
    }
  }
}

// Compute Galileo Satellite Position (virtual)
////////////////////////////////////////////////////////////////////////////
t_irc t_ephGal::position(int GPSweek, double GPSweeks, double* xc, double* vv) const {

  static const double omegaEarth = 7292115.1467e-11;
  static const double gmWGS = 398.6004418e12;

  memset(xc, 0, 6*sizeof(double));
  memset(vv, 0, 3*sizeof(double));

  double a0 = _sqrt_A * _sqrt_A;
  if (a0 == 0) {
    return failure;
  }

  double n0 = sqrt(gmWGS/(a0*a0*a0));

  bncTime tt(GPSweek, GPSweeks);
  double tk = tt - bncTime(_TOC.gpsw(), _TOEsec);

  double n  = n0 + _Delta_n;
  double M  = _M0 + n*tk;
  double E  = M;
  double E_last;
  int    nLoop = 0;
  do {
    E_last = E;
    E = M + _e*sin(E);

    if (++nLoop == 100) {
      return failure;
    }
  } 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*_TOEsec;

  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 = tt - _TOC;
  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[3] -= 4.442807309e-10 * _e * sqrt(a0) *sin(E);

  xc[4] = _clock_drift + _clock_driftrate*tc;
  xc[5] = _clock_driftrate;

  return success;
}

// Health status of Galileo Ephemeris (virtual)
////////////////////////////////////////////////////////////////////////////
unsigned int t_ephGal::isUnhealthy() const {
  if (_E5aHS  == 1 || _E5aHS  == 3 ||
      _E5bHS  == 1 || _E5bHS  == 3 ||
      _E1_bHS == 1 || _E1_bHS == 3 ) {
    return 1;
  }
  if (_e5aDataInValid ||
      _e5bDataInValid ||
      _e1DataInValid) {
    return 1;
  }
  if (_SISA == 255.0) {
    return 1;
  }
  /*
   * SDD v1.3: SHS=2 leads to a newly-defined "EOM" status.
   * It also means that the satellite signal may be used for PNT.
  if (_E5aHS  == 2 ||
      _E5bHS  == 2 ||
      _E1_bHS == 2 ) {
    return 1;
  }
  */
  return 0;
}

// RINEX Format String
//////////////////////////////////////////////////////////////////////////////
QString t_ephGal::toString(double version) const {

  QString navStr = navTypeString(_navType, _prn, version);
  QString rnxStr = navStr + rinexDateStr(_TOC, _prn, version);

  QTextStream out(&rnxStr);

  out << QString("%1%2%3\n")
    .arg(_clock_bias,      19, 'e', 12)
    .arg(_clock_drift,     19, 'e', 12)
    .arg(_clock_driftrate, 19, 'e', 12);

  QString fmt = version < 3.0 ? "   %1%2%3%4\n" : "    %1%2%3%4\n";
  // =====================
  // BROADCAST ORBIT - 1
  // =====================
  out << QString(fmt)
    .arg(_IODnav,  19, 'e', 12)
    .arg(_Crs,     19, 'e', 12)
    .arg(_Delta_n, 19, 'e', 12)
    .arg(_M0,      19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 2
  // =====================
  out << QString(fmt)
    .arg(_Cuc,    19, 'e', 12)
    .arg(_e,      19, 'e', 12)
    .arg(_Cus,    19, 'e', 12)
    .arg(_sqrt_A, 19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 3
  // =====================
  out << QString(fmt)
    .arg(_TOEsec, 19, 'e', 12)
    .arg(_Cic,    19, 'e', 12)
    .arg(_OMEGA0, 19, 'e', 12)
    .arg(_Cis,    19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 4
  // =====================
  out << QString(fmt)
    .arg(_i0,       19, 'e', 12)
    .arg(_Crc,      19, 'e', 12)
    .arg(_omega,    19, 'e', 12)
    .arg(_OMEGADOT, 19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 5
  // =====================
  int    dataSource = 0;
  int    SVhealth   = 0;
  double BGD_1_5A   = _BGD_1_5A;
  double BGD_1_5B   = _BGD_1_5B;
  if (_fnav) {
    dataSource |= (1<<1);
    dataSource |= (1<<8);
    BGD_1_5B = 0.0;
    // SVhealth
    //   Bit 3  : E5a DVS
    if (_e5aDataInValid) {
      SVhealth |= (1<<3);
    }
    //   Bit 4-5: E5a HS
    if (_E5aHS == 1.0) {
      SVhealth |= (1<<4);
    }
    else if (_E5aHS == 2.0) {
      SVhealth |= (1<<5);
    }
    else if (_E5aHS  == 3.0) {
      SVhealth |= (1<<4);
      SVhealth |= (1<<5);
    }
  }
  else if(_inav) {
    // Bit 2 and 0 are set because from MT1046 the data source cannot be determined
    // and RNXv3.03 says both can be set if the navigation messages were merged
    dataSource |= (1<<0);
    dataSource |= (1<<2);
    dataSource |= (1<<9);
    // SVhealth
    //   Bit 0  : E1-B DVS
    if (_e1DataInValid) {
      SVhealth |= (1<<0);
    }
    //   Bit 1-2: E1-B HS
    if      (_E1_bHS == 1.0) {
      SVhealth |= (1<<1);
    }
    else if (_E1_bHS == 2.0) {
      SVhealth |= (1<<2);
    }
    else if (_E1_bHS == 3.0) {
      SVhealth |= (1<<1);
      SVhealth |= (1<<2);
    }
    //   Bit 3  : E5a DVS
    if (_e5aDataInValid) {
      SVhealth |= (1<<3);
    }
    //   Bit 4-5: E5a HS
    if      (_E5aHS == 1.0) {
      SVhealth |= (1<<4);
    }
    else if (_E5aHS == 2.0) {
      SVhealth |= (1<<5);
    }
    else if (_E5aHS == 3.0) {
      SVhealth |= (1<<4);
      SVhealth |= (1<<5);
    }
    //   Bit 6  : E5b DVS
    if (_e5bDataInValid) {
      SVhealth |= (1<<6);
    }
    //   Bit 7-8: E5b HS
    if      (_E5bHS == 1.0) {
      SVhealth |= (1<<7);
    }
    else if (_E5bHS == 2.0) {
      SVhealth |= (1<<8);
    }
    else if (_E5bHS == 3.0) {
      SVhealth |= (1<<7);
      SVhealth |= (1<<8);
    }
  }

  out << QString(fmt)
    .arg(_IDOT,              19, 'e', 12)
    .arg(double(dataSource), 19, 'e', 12)
    .arg(_TOEweek + 1024.0,  19, 'e', 12)
    .arg(0.0,                19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 6
  // =====================
  out << QString(fmt)
    .arg(_SISA,            19, 'e', 12)
    .arg(double(SVhealth), 19, 'e', 12)
    .arg(BGD_1_5A,         19, 'e', 12)
    .arg(BGD_1_5B,         19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 7
  // =====================
  double tot = _TOT;
  if (tot == 0.9999e9 && version < 3.0) {
    tot = 0.0;
  }
  out << QString(fmt)
    .arg(tot,     19, 'e', 12)
    .arg("",      19, QChar(' '))
    .arg("",      19, QChar(' '))
    .arg("",      19, QChar(' '));

  return rnxStr;
}

// Constructor
//////////////////////////////////////////////////////////////////////////////
t_ephSBAS::t_ephSBAS(double rnxVersion, const QStringList& lines) {

  const int nLines = 4;

  if (lines.size() != nLines) {
    _checkState = bad;
    return;
  }

  // RINEX Format
  // ------------
  int fieldLen = 19;

  int pos[4];
  pos[0] = (rnxVersion <= 2.12) ?  3 :  4;
  pos[1] = pos[0] + fieldLen;
  pos[2] = pos[1] + fieldLen;
  pos[3] = pos[2] + fieldLen;

  // Read four lines
  // ---------------
  for (int iLine = 0; iLine < nLines; iLine++) {
    QString line = lines[iLine];

    if      ( iLine == 0 ) {
      QTextStream in(line.left(pos[1]).toLatin1());

      int    year, month, day, hour, min;
      double sec;

      QString prnStr, n;
      in >> prnStr;
      if (prnStr.size() == 1 && prnStr[0] == 'S') {
        in >> n;
        prnStr.append(n);
      }
      in >> year >> month >> day >> hour >> min >> sec;
      if (prnStr.at(0) == 'S') {
        _prn.set('S', prnStr.mid(1).toInt());
      }
      else {
        _prn.set('S', prnStr.toInt());
      }

      if      (year <  80) {
        year += 2000;
      }
      else if (year < 100) {
        year += 1900;
      }

      _TOC.set(year, month, day, hour, min, sec);

      if ( readDbl(line, pos[1], fieldLen, _agf0 ) ||
           readDbl(line, pos[2], fieldLen, _agf1 ) ||
           readDbl(line, pos[3], fieldLen, _TOT  ) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 1
    // =====================
    else if      ( iLine == 1 ) {
      if ( readDbl(line, pos[0], fieldLen, _x_pos         ) ||
           readDbl(line, pos[1], fieldLen, _x_velocity    ) ||
           readDbl(line, pos[2], fieldLen, _x_acceleration) ||
           readDbl(line, pos[3], fieldLen, _health        ) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 2
    // =====================
    else if ( iLine == 2 ) {
      if ( readDbl(line, pos[0], fieldLen, _y_pos           ) ||
           readDbl(line, pos[1], fieldLen, _y_velocity      ) ||
           readDbl(line, pos[2], fieldLen, _y_acceleration  ) ||
           readDbl(line, pos[3], fieldLen, _ura             ) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 3
    // =====================
    else if ( iLine == 3 ) {
      double iodn;
      if ( readDbl(line, pos[0], fieldLen, _z_pos         )  ||
           readDbl(line, pos[1], fieldLen, _z_velocity    )  ||
           readDbl(line, pos[2], fieldLen, _z_acceleration)  ||
           readDbl(line, pos[3], fieldLen, iodn           ) ) {
        _checkState = bad;
        return;
      } else {
        _IODN = int(iodn);
      }
    }
  }

  _x_pos          *= 1.e3;
  _y_pos          *= 1.e3;
  _z_pos          *= 1.e3;
  _x_velocity     *= 1.e3;
  _y_velocity     *= 1.e3;
  _z_velocity     *= 1.e3;
  _x_acceleration *= 1.e3;
  _y_acceleration *= 1.e3;
  _z_acceleration *= 1.e3;
}

// IOD of SBAS Ephemeris (virtual)
////////////////////////////////////////////////////////////////////////////

unsigned int t_ephSBAS::IOD() const {
  unsigned char buffer[80];
  int size = 0;
  int numbits = 0;
  long long bitbuffer = 0;
  unsigned char *startbuffer = buffer;

  SBASADDBITSFLOAT(30, this->_x_pos, 0.08)
  SBASADDBITSFLOAT(30, this->_y_pos, 0.08)
  SBASADDBITSFLOAT(25, this->_z_pos, 0.4)
  SBASADDBITSFLOAT(17, this->_x_velocity, 0.000625)
  SBASADDBITSFLOAT(17, this->_y_velocity, 0.000625)
  SBASADDBITSFLOAT(18, this->_z_velocity, 0.004)
  SBASADDBITSFLOAT(10, this->_x_acceleration, 0.0000125)
  SBASADDBITSFLOAT(10, this->_y_acceleration, 0.0000125)
  SBASADDBITSFLOAT(10, this->_z_acceleration, 0.0000625)
  SBASADDBITSFLOAT(12, this->_agf0, 1.0/static_cast<double>(1<<30)/static_cast<double>(1<<1))
  SBASADDBITSFLOAT(8, this->_agf1, 1.0/static_cast<double>(1<<30)/static_cast<double>(1<<10))
  SBASADDBITS(5,0); // the last byte is filled by 0-bits to obtain a length of an integer multiple of 8

  return CRC24(size, startbuffer);
}

// Compute SBAS Satellite Position (virtual)
////////////////////////////////////////////////////////////////////////////
t_irc t_ephSBAS::position(int GPSweek, double GPSweeks, double* xc, double* vv) const {

  bncTime tt(GPSweek, GPSweeks);
  double  dt = tt - _TOC;

  xc[0] = _x_pos + _x_velocity * dt + _x_acceleration * dt * dt / 2.0;
  xc[1] = _y_pos + _y_velocity * dt + _y_acceleration * dt * dt / 2.0;
  xc[2] = _z_pos + _z_velocity * dt + _z_acceleration * dt * dt / 2.0;

  vv[0] = _x_velocity + _x_acceleration * dt;
  vv[1] = _y_velocity + _y_acceleration * dt;
  vv[2] = _z_velocity + _z_acceleration * dt;

  xc[3] = _agf0 + _agf1 * dt;

  xc[4] = _agf1;
  xc[5] = 0.0;

  return success;
}

// Health status of SBAS Ephemeris (virtual)
////////////////////////////////////////////////////////////////////////////
unsigned int t_ephSBAS::isUnhealthy() const {

  // Bit 5
  bool URAindexIs15 = (int(_health) & (1<<5));
  if (URAindexIs15) {
    // in this case it is recommended
    // to set the bits 0,1,2,3 to 1 (MT17health = 15)
    return 1;
  }

  // Bit 0-3
  int   MT17health = (int(_health)) & (0x0f);
  if (MT17health) {
    return 1;
  }

  // Bit 4
  //  bool MT17HealthIsUnavailable = (int(_health) & (1<<4));
  //  is not used because the MT17health bits can be independently set if URA index is 15

  return 0;
}


// RINEX Format String
//////////////////////////////////////////////////////////////////////////////
QString t_ephSBAS::toString(double version) const {

  QString navStr = navTypeString(_navType, _prn, version);
  QString rnxStr = navStr + rinexDateStr(_TOC, _prn, version);

  QTextStream out(&rnxStr);

  out << QString("%1%2%3\n")
    .arg(_agf0, 19, 'e', 12)
    .arg(_agf1, 19, 'e', 12)
    .arg(_TOT,  19, 'e', 12);

  QString fmt = version < 3.0 ? "   %1%2%3%4\n" : "    %1%2%3%4\n";
  // =====================
  // BROADCAST ORBIT - 1
  // =====================
  out << QString(fmt)
    .arg(1.e-3*_x_pos,          19, 'e', 12)
    .arg(1.e-3*_x_velocity,     19, 'e', 12)
    .arg(1.e-3*_x_acceleration, 19, 'e', 12)
    .arg(_health,               19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 2
  // =====================
  out << QString(fmt)
    .arg(1.e-3*_y_pos,          19, 'e', 12)
    .arg(1.e-3*_y_velocity,     19, 'e', 12)
    .arg(1.e-3*_y_acceleration, 19, 'e', 12)
    .arg(_ura,                  19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 3
  // =====================
  out << QString(fmt)
    .arg(1.e-3*_z_pos,          19, 'e', 12)
    .arg(1.e-3*_z_velocity,     19, 'e', 12)
    .arg(1.e-3*_z_acceleration, 19, 'e', 12)
    .arg(double(_IODN),         19, 'e', 12);

  return rnxStr;
}

// Constructor
//////////////////////////////////////////////////////////////////////////////
t_ephBDS::t_ephBDS(double rnxVersion, const QStringList& lines) {

  int nLines = 8;

  if (navType() == t_eph::CNV1 ||
      navType() == t_eph::CNV2) {
    nLines += 2;
  }
  if (navType() == t_eph::CNV3) {
    nLines += 1;
  }

  if (lines.size() != nLines) {
    _checkState = bad;
    return;
  }

  // RINEX Format
  // ------------
  int fieldLen = 19;

  int pos[4];
  pos[0] = (rnxVersion <= 2.12) ?  3 :  4;
  pos[1] = pos[0] + fieldLen;
  pos[2] = pos[1] + fieldLen;
  pos[3] = pos[2] + fieldLen;

  // Read eight lines
  // ----------------
  for (int iLine = 0; iLine < nLines; iLine++) {
    QString line = lines[iLine];

    if      ( iLine == 0 ) {
      QTextStream in(line.left(pos[1]).toLatin1());

      int    year, month, day, hour, min;
      double sec;

      QString prnStr, n;
      in >> prnStr;
      if (prnStr.size() == 1 && prnStr[0] == 'C') {
        in >> n;
        prnStr.append(n);
      }
      in >> year >> month >> day >> hour >> min >> sec;
      if (prnStr.at(0) == 'C') {
        _prn.set('C', prnStr.mid(1).toInt());
      }
      else {
        _prn.set('C', prnStr.toInt());
      }

      if      (year <  80) {
        year += 2000;
      }
      else if (year < 100) {
        year += 1900;
      }

      _TOC.setBDS(year, month, day, hour, min, sec);

      if ( readDbl(line, pos[1], fieldLen, _clock_bias     ) ||
           readDbl(line, pos[2], fieldLen, _clock_drift    ) ||
           readDbl(line, pos[3], fieldLen, _clock_driftrate) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 1
    // =====================
    else if      ( iLine == 1 ) {
      double aode;
      if ( readDbl(line, pos[0], fieldLen, aode    ) ||
           readDbl(line, pos[1], fieldLen, _Crs    ) ||
           readDbl(line, pos[2], fieldLen, _Delta_n) ||
           readDbl(line, pos[3], fieldLen, _M0     ) ) {
        _checkState = bad;
        return;
      }
      _AODE = int(aode);
    }
    // =====================
    // BROADCAST ORBIT - 2
    // =====================
    else if ( iLine == 2 ) {
      if ( readDbl(line, pos[0], fieldLen, _Cuc   ) ||
           readDbl(line, pos[1], fieldLen, _e     ) ||
           readDbl(line, pos[2], fieldLen, _Cus   ) ||
           readDbl(line, pos[3], fieldLen, _sqrt_A) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 3
    // =====================
    else if ( iLine == 3 ) {
      if ( readDbl(line, pos[0], fieldLen, _TOEsec )  ||
           readDbl(line, pos[1], fieldLen, _Cic   )  ||
           readDbl(line, pos[2], fieldLen, _OMEGA0)  ||
           readDbl(line, pos[3], fieldLen, _Cis   ) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 4
    // =====================
    else if ( iLine == 4 ) {
      if ( readDbl(line, pos[0], fieldLen, _i0      ) ||
           readDbl(line, pos[1], fieldLen, _Crc     ) ||
           readDbl(line, pos[2], fieldLen, _omega   ) ||
           readDbl(line, pos[3], fieldLen, _OMEGADOT) ) {
        _checkState = bad;
        return;
      }
    }
    // =====================
    // BROADCAST ORBIT - 5
    // =====================
    else if ( iLine == 5 ) {

      if (navType() == t_eph::CNV1 ||
          navType() == t_eph::CNV2 ||
          navType() == t_eph::CNV3 ) {
        if ( readDbl(line, pos[0], fieldLen, _IDOT       ) ||
             readDbl(line, pos[1], fieldLen, _Delta_n_dot) ||
             readDbl(line, pos[2], fieldLen, _satType    ) ||
             readDbl(line, pos[3], fieldLen, _top        ) ) {
          _checkState = bad;
          return;
        }
      }
      else { // D1, D2, undefined
        if ( readDbl(line, pos[0], fieldLen, _IDOT    ) ||
             readDbl(line, pos[2], fieldLen, _BDTweek)) {
          _checkState = bad;
          return;
        }
      }
    }
    // =====================
    // BROADCAST ORBIT - 6
    // =====================
    else if ( iLine == 6 ) {
      if (navType() == t_eph::CNV1 ||
          navType() == t_eph::CNV2 ||
          navType() == t_eph::CNV3 ) {
        if ( readDbl(line, pos[0], fieldLen, _SISAI_oe  ) ||
             readDbl(line, pos[1], fieldLen, _SISAI_ocb ) ||
             readDbl(line, pos[2], fieldLen, _SISAI_oc1 ) ||
             readDbl(line, pos[3], fieldLen, _SISAI_oc2  ) ) {
          _checkState = bad;
          return;
        }
      }
      else { // D1, D2, undefined
        double SatH1;
        if ( readDbl(line, pos[0], fieldLen, _URA ) ||
             readDbl(line, pos[1], fieldLen, SatH1) ||
             readDbl(line, pos[2], fieldLen, _TGD1) ||
             readDbl(line, pos[3], fieldLen, _TGD2) ) {
          _checkState = bad;
          return;
        }
        _SatH1 = int(SatH1);
      }
    }
    // =====================
    // BROADCAST ORBIT - 7
    // =====================
    else if ( iLine == 7 ) {
      if (navType() == t_eph::CNV1) {
        if ( readDbl(line, pos[0], fieldLen, _ISC_B1Cd) ||
             readDbl(line, pos[2], fieldLen, _TGD_B1Cp) ||
             readDbl(line, pos[3], fieldLen, _TGD_B2ap) ) {
          _checkState = bad;
          return;
        }
      }
      else if (navType() == t_eph::CNV2) {
        if ( readDbl(line, pos[1], fieldLen, _ISC_B2ad) ||
             readDbl(line, pos[2], fieldLen, _TGD_B1Cp) ||
             readDbl(line, pos[3], fieldLen, _TGD_B2ap) ) {
          _checkState = bad;
          return;
        }
      }
      else if (navType() == t_eph::CNV3) {
        double health;
        if ( readDbl(line, pos[0], fieldLen, _SISMAI        ) ||
             readDbl(line, pos[1], fieldLen,  health        ) ||
             readDbl(line, pos[2], fieldLen, _INTEGRITYF_B2b) ||
             readDbl(line, pos[3], fieldLen, _TGD_B2bI)     )  {
          _checkState = bad;
          return;
        }
        _health = int(health);
      }
      else { // D1, D2 or undefined
        double aodc;
        if ( readDbl(line, pos[0], fieldLen, _TOT) ||
             readDbl(line, pos[1], fieldLen, aodc) ) {
          _checkState = bad;
          return;
        }
        if (_TOT == 0.9999e9) {  // 0.9999e9 means not known (RINEX standard)
          _TOT = _TOEsec;
        }
        _AODC = int(aodc);
      }
    }
    // =====================
    // BROADCAST ORBIT - 8
    // =====================
    else if ( iLine == 8 ) {
      double health;
      if      (navType() == t_eph::CNV1) {
        if ( readDbl(line, pos[0], fieldLen, _SISMAI        ) ||
             readDbl(line, pos[1], fieldLen,  health        ) ||
             readDbl(line, pos[2], fieldLen, _INTEGRITYF_B1C) ||
             readDbl(line, pos[3], fieldLen, _IODC)     )  {
          _checkState = bad;
          return;
        }
        _health = int(health);
      }
      else if (navType() == t_eph::CNV2) {
        if ( readDbl(line, pos[0], fieldLen, _SISMAI           ) ||
             readDbl(line, pos[1], fieldLen,  health           ) ||
             readDbl(line, pos[2], fieldLen, _INTEGRITYF_B2aB1C) ||
             readDbl(line, pos[3], fieldLen, _IODC)            )  {
          _checkState = bad;
          return;
        }
        _health = int(health);
      }
      else if (navType() == t_eph::CNV3) {
        if ( readDbl(line, pos[0], fieldLen, _TOT)) {
          _checkState = bad;
          return;
        }
      }

    }
    // =====================
    // BROADCAST ORBIT - 9
    // =====================
    else if ( iLine == 9 ) {

      if      (navType() == t_eph::CNV1 ||
               navType() == t_eph::CNV2) {
        if ( readDbl(line, pos[0], fieldLen, _TOT) ||
             readDbl(line, pos[3], fieldLen, _IODE) ) {
          _checkState = bad;
          return;
        }
      }

    }
  }

   _TOE.setBDS(int(_BDTweek), _TOEsec);
  // remark: actually should be computed from second_tot
  //         but it seems to be unreliable in RINEX files
  //_TOT = _TOC.bdssec();
}

// IOD of BDS Ephemeris (virtual)
////////////////////////////////////////////////////////////////////////////
unsigned int t_ephBDS::IOD() const {
  return (int(_TOC.gpssec())/720) % 240;   //return (int(_TOEsec)/720) % 240;
}

// Compute BDS Satellite Position (virtual)
//////////////////////////////////////////////////////////////////////////////
t_irc t_ephBDS::position(int GPSweek, double GPSweeks, double* xc, double* vv) const {

  static const double gmBDS    = 398.6004418e12;
  static const double omegaBDS = 7292115.0000e-11;

  xc[0] = xc[1] = xc[2] = xc[3] = 0.0;
  vv[0] = vv[1] = vv[2] = 0.0;

  bncTime tt(GPSweek, GPSweeks);

  if (_sqrt_A == 0) {
    return failure;
  }
  double a0 = _sqrt_A * _sqrt_A;

  double n0 = sqrt(gmBDS/(a0*a0*a0));
  double tk = tt - _TOE;
  double n  = n0 + _Delta_n;
  double M  = _M0 + n*tk;
  double E  = M;
  double E_last;
  int    nLoop = 0;
  do {
    E_last = E;
    E = M + _e*sin(E);

    if (++nLoop == 100) {
      return failure;
    }
  } while ( fabs(E-E_last)*a0 > 0.001 );

  double v      = atan2(sqrt(1-_e*_e) * sin(E), cos(E) - _e);
  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 toesec = (_TOE.gpssec() - 14.0);
  double sinom = 0;
  double cosom = 0;
  double sini  = 0;
  double cosi  = 0;

  // 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 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;

  const double iMaxGEO = 10.0 / 180.0 * M_PI;

  // MEO/IGSO satellite
  // ------------------
  if (_i0 > iMaxGEO) {
    double OM = _OMEGA0 + (_OMEGADOT - omegaBDS)*tk - omegaBDS*toesec;

    sinom = sin(OM);
    cosom = cos(OM);
    sini  = sin(i);
    cosi  = cos(i);

    xc[0] = xp*cosom - yp*cosi*sinom;
    xc[1] = xp*sinom + yp*cosi*cosom;
    xc[2] = yp*sini;

    // Velocity
    // --------

    double dotom = _OMEGADOT - t_CST::omega;

    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;

  }

  // GEO satellite
  // -------------
  else {
    double OM    = _OMEGA0 + _OMEGADOT*tk - omegaBDS*toesec;
    double ll    = omegaBDS*tk;

    sinom = sin(OM);
    cosom = cos(OM);
    sini  = sin(i);
    cosi  = cos(i);

    double xx = xp*cosom - yp*cosi*sinom;
    double yy = xp*sinom + yp*cosi*cosom;
    double zz = yp*sini;

    Matrix RX = BNC_PPP::t_astro::rotX(-5.0 / 180.0 * M_PI);
    Matrix RZ = BNC_PPP::t_astro::rotZ(ll);

    ColumnVector X1(3); X1 << xx << yy << zz;
    ColumnVector X2 = RZ*RX*X1;

    xc[0] = X2(1);
    xc[1] = X2(2);
    xc[2] = X2(3);

    double dotom = _OMEGADOT;

    double vx  = cosom   *dotx  - cosi*sinom   *doty
               - xp*sinom*dotom - yp*cosi*cosom*dotom
                                + yp*sini*sinom*doti;

    double vy  = sinom   *dotx  + cosi*cosom   *doty
               + xp*cosom*dotom - yp*cosi*sinom*dotom
                                - yp*sini*cosom*doti;

    double vz  = sini    *doty  + yp*cosi      *doti;

    ColumnVector V(3); V << vx << vy << vz;

    Matrix RdotZ(3,3);
    double C = cos(ll);
    double S = sin(ll);
    Matrix UU(3,3);
    UU[0][0] =  -S;  UU[0][1] =  +C;  UU[0][2] = 0.0;
    UU[1][0] =  -C;  UU[1][1] =  -S;  UU[1][2] = 0.0;
    UU[2][0] = 0.0;  UU[2][1] = 0.0;  UU[2][2] = 0.0;
    RdotZ = omegaBDS * UU;

    ColumnVector VV(3);
    VV = RZ*RX*V + RdotZ*RX*X1;

    vv[0] = VV(1);
    vv[1] = VV(2);
    vv[2] = VV(3);
  }

  double tc = tt - _TOC;
  xc[3] = _clock_bias + _clock_drift*tc + _clock_driftrate*tc*tc;

//  dotC  = _clock_drift + _clock_driftrate*tc
//        - 4.442807309e-10*_e * sqrt(a0) * cos(E) * dEdM * n;

  // Relativistic Correction
  // -----------------------
  xc[3] -= 4.442807309e-10 * _e * sqrt(a0) *sin(E);

  xc[4] = _clock_drift + _clock_driftrate*tc;
  xc[5] = _clock_driftrate;

  return success;
}


// Health status of SBAS Ephemeris (virtual)
////////////////////////////////////////////////////////////////////////////
unsigned int t_ephBDS::isUnhealthy() const {

  if (navType() == t_eph::CNV1 ||
      navType() == t_eph::CNV2 ||
      navType() == t_eph::CNV3) {
    return static_cast<unsigned int>(_health);
  }

  return static_cast<unsigned int>(_SatH1);

}


// RINEX Format String
//////////////////////////////////////////////////////////////////////////////
QString t_ephBDS::toString(double version) const {

  QString navStr = navTypeString(_navType, _prn, version);
  QString rnxStr = navStr + rinexDateStr(_TOC-14.0, _prn, version);

  QTextStream out(&rnxStr);

  out << QString("%1%2%3\n")
    .arg(_clock_bias,      19, 'e', 12)
    .arg(_clock_drift,     19, 'e', 12)
    .arg(_clock_driftrate, 19, 'e', 12);

  QString fmt = version < 3.0 ? "   %1%2%3%4\n" : "    %1%2%3%4\n";
  // =====================
  // BROADCAST ORBIT - 1
  // =====================
  out << QString(fmt)
    .arg(double(_AODE), 19, 'e', 12)
    .arg(_Crs,          19, 'e', 12)
    .arg(_Delta_n,      19, 'e', 12)
    .arg(_M0,           19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 2
  // =====================
  out << QString(fmt)
    .arg(_Cuc,    19, 'e', 12)
    .arg(_e,      19, 'e', 12)
    .arg(_Cus,    19, 'e', 12)
    .arg(_sqrt_A, 19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 3
  // =====================
  out << QString(fmt)
    .arg(_TOEsec, 19, 'e', 12)
    .arg(_Cic,    19, 'e', 12)
    .arg(_OMEGA0, 19, 'e', 12)
    .arg(_Cis,    19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 4
  // =====================
  out << QString(fmt)
    .arg(_i0,       19, 'e', 12)
    .arg(_Crc,      19, 'e', 12)
    .arg(_omega,    19, 'e', 12)
    .arg(_OMEGADOT, 19, 'e', 12);
  // =====================
  // BROADCAST ORBIT - 5
  // =====================
  if (navType() == t_eph::CNV1 ||
      navType() == t_eph::CNV2 ||
      navType() == t_eph::CNV3 ) {
    out << QString(fmt)
      .arg(_IDOT,        19, 'e', 12)
      .arg(_Delta_n_dot, 19, 'e', 12)
      .arg(_satType,     19, 'e', 12)
      .arg(_top,         19, 'e', 12);
  }
  else { // D1, D2, undefined
    out << QString(fmt)
      .arg(_IDOT,    19, 'e', 12)
      .arg("",            19, QChar(' '))
      .arg(_BDTweek, 19, 'e', 12)
      .arg("",            19, QChar(' '));
  }
  // =====================
  // BROADCAST ORBIT - 6
  // =====================
  if (navType() == t_eph::CNV1 ||
      navType() == t_eph::CNV2 ||
      navType() == t_eph::CNV3 ) {
    out << QString(fmt)
      .arg(_SISAI_oe,  19, 'e', 12)
      .arg(_SISAI_ocb, 19, 'e', 12)
      .arg(_SISAI_oc1, 19, 'e', 12)
      .arg(_SISAI_oc2, 19, 'e', 12);
  }
  else { // D1, D2, undefined
    out << QString(fmt)
      .arg(_URA,           19, 'e', 12)
      .arg(double(_SatH1), 19, 'e', 12)
      .arg(_TGD1,          19, 'e', 12)
      .arg(_TGD2,          19, 'e', 12);
  }
  // =====================
  // BROADCAST ORBIT - 7
  // =====================
  if      (navType() == t_eph::CNV1) {
    out << QString(fmt)
      .arg(_ISC_B1Cd, 19, 'e', 12)
      .arg("",        19, QChar(' '))
      .arg(_TGD_B1Cp, 19, 'e', 12)
      .arg(_TGD_B2ap, 19, 'e', 12);
  }
  else if (navType() == t_eph::CNV2) {
    out << QString(fmt)
      .arg("",        19, QChar(' '))
      .arg(_ISC_B2ad, 19, 'e', 12)
      .arg(_TGD_B1Cp, 19, 'e', 12)
      .arg(_TGD_B2ap, 19, 'e', 12);
  }
  else if (navType() == t_eph::CNV3) {
    out << QString(fmt)
      .arg(_SISMAI,         19, 'e', 12)
      .arg(double(_health), 19, 'e', 12)
      .arg(_INTEGRITYF_B2b, 19, 'e', 12)
      .arg(_TGD_B2bI,       19, 'e', 12);
  }
  else { // D1, D2, undefined
    double tots = 0.0;
    if (_receptDateTime.isValid()) {// RTCM stream input
      tots = _TOE.bdssec();
    }
    else { // RINEX input
      tots = _TOT;
    }
    out << QString(fmt)
      .arg(tots,          19, 'e', 12)
      .arg(double(_AODC), 19, 'e', 12)
      .arg("",            19, QChar(' '))
      .arg("",            19, QChar(' '));
  }

  // =====================
  // BROADCAST ORBIT - 8
  // =====================
  if      (navType() == t_eph::CNV1) {
    out << QString(fmt)
      .arg(_SISMAI,         19, 'e', 12)
      .arg(double(_health), 19, 'e', 12)
      .arg(_INTEGRITYF_B1C, 19, 'e', 12)
      .arg(_IODC,           19, 'e', 12);
  }
  else if (navType() == t_eph::CNV2) {
    out << QString(fmt)
      .arg(_SISMAI,            19, 'e', 12)
      .arg(double(_health),    19, 'e', 12)
      .arg(_INTEGRITYF_B2aB1C, 19, 'e', 12)
      .arg(_IODC,              19, 'e', 12);
  }
  else if (navType() == t_eph::CNV3) {
    out << QString(fmt)
      .arg(_TOT,          19, 'e', 12)
      .arg("",            19, QChar(' '))
      .arg("",            19, QChar(' '))
      .arg("",            19, QChar(' '));
  }

  // =====================
  // BROADCAST ORBIT - 9
  // =====================
  if      (navType() == t_eph::CNV1 ||
           navType() == t_eph::CNV2) {
    out << QString(fmt)
      .arg(_TOT,          19, 'e', 12)
      .arg("",            19, QChar(' '))
      .arg("",            19, QChar(' '))
      .arg(_IODE,         19, 'e', 12);
  }


  return rnxStr;
}