/* -------------------------------------------------------------------------
 * BKG NTRIP Server
 * -------------------------------------------------------------------------
 *
 * Class:      bncRtnetUploadCaster
 *
 * Purpose:    Connection to NTRIP Caster
 *
 * Author:     L. Mervart
 *
 * Created:    29-Mar-2011
 *
 * Changes:
 *
 * -----------------------------------------------------------------------*/

#include <math.h>
#include "bncrtnetuploadcaster.h"
#include "bncsettings.h"
#include "bncephuser.h"
#include "bncclockrinex.h"
#include "bncbiassinex.h"
#include "bncsp3.h"
#include "gnss.h"
#include "bncutils.h"

using namespace std;

// Constructor
////////////////////////////////////////////////////////////////////////////
bncRtnetUploadCaster::bncRtnetUploadCaster(const QString& mountpoint,
    const QString& outHost, int outPort,
    const QString& ntripVersion,
    const QString& userName, const QString& password,
    const QString& crdTrafo, const QString& ssrFormat, bool CoM, const QString& sp3FileName,
    const QString& rnxFileName, const QString& bsxFileName, int PID, int SID, int IOD, int iRow) :
    bncUploadCaster(mountpoint, outHost, outPort, ntripVersion, userName, password, iRow, 0) {

    if (!mountpoint.isEmpty()) {
        _casterID += mountpoint;
    }
    if (!outHost.isEmpty()) {
        _casterID += " " + outHost;
        if (outPort) {
            _casterID += ":" + QString("%1").arg(outPort, 10);
        }
    }
    if (!crdTrafo.isEmpty()) {
        _casterID += " " + crdTrafo;
    }
    if (!sp3FileName.isEmpty()) {
        _casterID += " " + sp3FileName;
    }
    if (!rnxFileName.isEmpty()) {
        _casterID += " " + rnxFileName;
    }

    if (!bsxFileName.isEmpty()) {
        _casterID += " " + bsxFileName;
    }

    _crdTrafoStr = crdTrafo;

    _ssrFormat = ssrFormat;

    _ssrCorr = 0;
    if (_ssrFormat == "IGS-SSR") {
        _ssrCorr = new SsrCorrIgs();
    }
    else if (_ssrFormat == "RTCM-SSR") {
        _ssrCorr = new SsrCorrRtcm();
    }
    else if (ssrFormat == "RTCM-NEW-SSR") {
      _ssrCorr = new SsrCorrRtcmNew();
    }

    _CoM = CoM;
    _PID = PID;
    _SID = SID;
    _IOD = IOD;
    _phaseBiasInformationDecoded = false;

    // Member that receives the ephemeris
    // ----------------------------------
    _ephUser = new bncEphUser(true);

    bncSettings settings;
    QString intr      = settings.value("uploadIntr").toString();
    QStringList hlp   = settings.value("cmbStreams").toStringList();
    _samplRtcmEphCorr = settings.value("uploadSamplRtcmEphCorr").toString().split("sec").first().toDouble();

    if (hlp.size() > 1) { // combination stream upload
        _samplRtcmClkCorr = settings.value("cmbSampl").toString().split("sec").first().toDouble();
    }
    else { // single stream upload or sp3 file generation
        _samplRtcmClkCorr = 5.0; // default
    }
    _samplRtcmVtec = 60.0;
    _samplRtcmCrs = 60.0;
    int samplSp3    = settings.value("uploadSamplSp3").toString().split("sec").first().toInt();
    int samplClkRnx = settings.value("uploadSamplClkRnx").toInt();
    int samplBiaSnx = settings.value("uploadSamplBiaSnx").toInt();

    if (_samplRtcmEphCorr == 0.0) {
        _usedEph = 0;
    }
    else {
        _usedEph = new QMap<QString, const t_eph*>;
    }

    // RINEX writer
    // ------------
    if (!rnxFileName.isEmpty()) {
        _rnx = new bncClockRinex(rnxFileName, intr, samplClkRnx);
    }
    else {
        _rnx = 0;
    }

    // SP3 writer
    // ----------
    if (!sp3FileName.isEmpty()) {
        _sp3 = new bncSP3(sp3FileName, intr, samplSp3);
    }
    else {
        _sp3 = 0;
    }

    // SINEX writer
    // ------------
    if (!bsxFileName.isEmpty()) {
        _bsx = new bncBiasSinex(bsxFileName, intr, samplBiaSnx);
    }
    else {
        _bsx = 0;
    }


    // Set Transformation Parameters
    // -----------------------------
    // Transformation Parameters from ITRF2014 to ETRF2000
    // http://etrs89.ign.fr/pub/EUREF-TN-1-Mar-04-2024.pdf
    if (_crdTrafoStr == "ETRF2000") {
        _dx = 0.0552;
        _dy = 0.0527;
        _dz = -0.0836;

        _dxr = 0.0001;
        _dyr = 0.0001;
        _dzr = -0.0019;

        _ox = 0.002106;
        _oy = 0.012740;
        _oz = -0.020592;

        _oxr = 0.000081;
        _oyr = 0.000490;
        _ozr = -0.000792;

        _sc = 2.67;
        _scr = 0.11;

        _t0 = 2015.0;
    }
    // Transformation Parameters from ITRF2014 to GDA2020 (Ryan Ruddick, GA)
    else if (_crdTrafoStr == "GDA2020") {
        _dx = 0.0;
        _dy = 0.0;
        _dz = 0.0;

        _dxr = 0.0;
        _dyr = 0.0;
        _dzr = 0.0;

        _ox = 0.0;
        _oy = 0.0;
        _oz = 0.0;

        _oxr = 0.00150379;
        _oyr = 0.00118346;
        _ozr = 0.00120716;

        _sc = 0.0;
        _scr = 0.0;

        _t0 = 2020.0;
    }
    // Transformation Parameters from IGb14 to SIRGAS2000 (Thanks to Sonia Costa, BRA)
    // June 29 2020: TX:-0.0027 m  TY:-0.0025 m  TZ:-0.0042 m  SCL:1.20 (ppb) no rotations and no rates.*/
    else if (_crdTrafoStr == "SIRGAS2000") {
        _dx = -0.0027;
        _dy = -0.0025;
        _dz = -0.0042;

        _dxr = 0.0;
        _dyr = 0.0;
        _dzr = 0.0;

        _ox = 0.0;
        _oy = 0.0;
        _oz = 0.0;

        _oxr = 0.0;
        _oyr = 0.0;
        _ozr = 0.0;

        _sc = 1.2;
        _scr = 0.0;
        _t0 = 2000.0;
    }
    // Transformation Parameters from ITRF2014 to DREF91
    else if (_crdTrafoStr == "DREF91") {
        _dx = 0.0547;
        _dy = 0.0522;
        _dz = -0.0741;

        _dxr = 0.0001;
        _dyr = 0.0001;
        _dzr = -0.0019;
        // ERTF200  + rotation parameters (ETRF2000 => DREF91)
        _ox = 0.001701 + 0.000658;
        _oy = 0.010290 - 0.000208;
        _oz = -0.016632 + 0.000755;

        _oxr = 0.000081;
        _oyr = 0.000490;
        _ozr = -0.000729;

        _sc = 2.12;
        _scr = 0.11;

        _t0 = 2010.0;
    }
    else if (_crdTrafoStr == "Custom") {
        _dx = settings.value("trafo_dx").toDouble();
        _dy = settings.value("trafo_dy").toDouble();
        _dz = settings.value("trafo_dz").toDouble();
        _dxr = settings.value("trafo_dxr").toDouble();
        _dyr = settings.value("trafo_dyr").toDouble();
        _dzr = settings.value("trafo_dzr").toDouble();
        _ox = settings.value("trafo_ox").toDouble();
        _oy = settings.value("trafo_oy").toDouble();
        _oz = settings.value("trafo_oz").toDouble();
        _oxr = settings.value("trafo_oxr").toDouble();
        _oyr = settings.value("trafo_oyr").toDouble();
        _ozr = settings.value("trafo_ozr").toDouble();
        _sc = settings.value("trafo_sc").toDouble();
        _scr = settings.value("trafo_scr").toDouble();
        _t0 = settings.value("trafo_t0").toDouble();
    }
    // TODO: the following lines can be deleted if all parameters are updated regarding ITRF2020
    if (_crdTrafoStr == "ETRF2000" ||
        _crdTrafoStr == "GDA2020" ||
        _crdTrafoStr == "DREF91" ||
        _crdTrafoStr == "SIRGAS2000") {
        // Transformation Parameters from ITRF2020 to ITRF2014
        // from ITRF web site: https://itrf.ign.fr/en/solutions/transformations
        _dx14 = -0.0014;
        _dy14 = -0.0009;
        _dz14 = 0.0014;
        _dxr14 = 0.0;
        _dyr14 = -0.0001;
        _dzr14 = -0.0002;
        _ox14 = 0.0;
        _oy14 = 0.0;
        _oz14 = 0.0;
        _oxr14 = 0.0;
        _oyr14 = 0.0;
        _ozr14 = 0.0;
        _sc14 = -0.42;
        _scr14 = 0.0;
        _t014 = 2015.0;
    }
}

// Destructor
////////////////////////////////////////////////////////////////////////////
bncRtnetUploadCaster::~bncRtnetUploadCaster() {
    if (isRunning()) {
        wait();
    }
    delete _rnx;
    delete _sp3;
    delete _bsx;
    delete _ephUser;
    delete _usedEph;
    delete _ssrCorr;
}

//
////////////////////////////////////////////////////////////////////////////
void bncRtnetUploadCaster::decodeRtnetStream(char* buffer, int bufLen) {

    QMutexLocker locker(&_mutex);

    // Append to internal buffer
    // -------------------------
    _rtnetStreamBuffer.append(QByteArray(buffer, bufLen));

    // Select buffer part that contains last epoch
    // -------------------------------------------
    QStringList lines;
    int iEpoBeg = _rtnetStreamBuffer.lastIndexOf('*');   // begin of last epoch
    if (iEpoBeg == -1) {
        _rtnetStreamBuffer.clear();
        return;
    }
    _rtnetStreamBuffer = _rtnetStreamBuffer.mid(iEpoBeg);

    int iEpoEnd = _rtnetStreamBuffer.lastIndexOf("EOE"); // end   of last epoch
    if (iEpoEnd == -1) {
        return;
    }
    else {
        lines = _rtnetStreamBuffer.left(iEpoEnd).split('\n', Qt::SkipEmptyParts);
        _rtnetStreamBuffer = _rtnetStreamBuffer.mid(iEpoEnd + 3);
    }

    if (lines.size() < 2) {
        emit(newMessage(
            "bncRtnetUploadCaster: less than 2 lines to decode " + _casterID.toLatin1(), false));
        return;
    }

    // Keep the last unfinished line in buffer
    // ---------------------------------------
    int iLastEOL = _rtnetStreamBuffer.lastIndexOf('\n');
    if (iLastEOL != -1) {
        _rtnetStreamBuffer = _rtnetStreamBuffer.mid(iLastEOL + 1);
    }


    // Read first line (with epoch time)
    // ---------------------------------
    //QTextStream in(lines[0].toLatin1());
    QTextStream in(&lines[0], QIODevice::ReadOnly);
    QString hlp;
    int year, month, day, hour, min;
    double sec;
    in >> hlp >> year >> month >> day >> hour >> min >> sec;
    bncTime epoTime;
    epoTime.set(year, month, day, hour, min, sec);

    emit(newMessage(
        "bncRtnetUploadCaster: decode " + QByteArray(epoTime.datestr().c_str())
        + " " + QByteArray(epoTime.timestr().c_str()) + " "
        + _casterID.toLatin1(), false));

    struct SsrCorr::ClockOrbit co;
    memset(&co, 0, sizeof(co));
    co.EpochTime[CLOCKORBIT_SATGPS] = static_cast<int>(epoTime.gpssec());
    double gt = epoTime.gpssec() - gnumleap(year, month, day);
    if (_ssrFormat == "RTCM-SSR") {
        gt += 3 * 3600;
    }
    co.EpochTime[CLOCKORBIT_SATGLONASS] = static_cast<int>(fmod(gt, 86400.0));
    co.EpochTime[CLOCKORBIT_SATGALILEO] = static_cast<int>(epoTime.gpssec());
    co.EpochTime[CLOCKORBIT_SATQZSS] = static_cast<int>(epoTime.gpssec());
    co.EpochTime[CLOCKORBIT_SATSBAS] = static_cast<int>(epoTime.gpssec());
    co.EpochTime[CLOCKORBIT_SATBDS] = static_cast<int>(epoTime.bdssec());
    co.Supplied[_ssrCorr->COBOFS_CLOCK] = 1;
    co.Supplied[_ssrCorr->COBOFS_ORBIT] = 1;
    (_crdTrafoStr == "IGS20") ?
        co.SatRefDatum = _ssrCorr->DATUM_ITRF :
        co.SatRefDatum = _ssrCorr->DATUM_LOCAL;
    co.SSRIOD = _IOD;
    co.SSRProviderID = _PID; // 256 .. BKG,  257 ... EUREF
    co.SSRSolutionID = _SID;
    co.Supplied[_ssrCorr->COBOFS_CLOCK] = 1;
    co.Supplied[_ssrCorr->COBOFS_ORBIT] = 1;

    t_serviceCrs serviceCrs;
    t_rtcmCrs    rtcmCrs;
    if (_crdTrafoStr == "IGS20") {
        serviceCrs._CE = serviceCrs._coordinateEpoch = 0;
        int nc = _crdTrafoStr.length();
        if (nc > 31) { nc = 31; }
        for (int i = 0; i < nc; i++) {
            serviceCrs._name[i] =
                rtcmCrs._name[i] = _crdTrafoStr.toStdString()[i];
        }
        serviceCrs._name[nc] = 0;
        rtcmCrs._name[nc] = 0;
        rtcmCrs._anchor = 0; // global CRS
        rtcmCrs._plateNumber = 0; // unknown
        rtcmCrs._databaseLinks << "ISO.DATUM.979" << "ISO.CRS:980";
    }
    else {
        if (_crdTrafoStr != "Custom") {
            serviceCrs._coordinateEpoch = _t0;
            serviceCrs.setCEFromCoordinateEpoch();
            int nc = _crdTrafoStr.length();
            if (nc > 31) { nc = 31; }
            for (int i = 0; i < nc; i++) {
                serviceCrs._name[i] = _crdTrafoStr.toStdString()[i];
            }
            serviceCrs._name[nc] = 0;
            QString rtcmcrsname = _crdTrafoStr + QString("(%1)").arg(_t0, 4, 'd', 0);
            nc = rtcmcrsname.length();
            if (nc > 31) { nc = 31; }
            for (int i = 0; i < nc; i++) {
                rtcmCrs._name[i] = rtcmcrsname.toStdString()[i];
            }
            rtcmCrs._name[nc] = 0;
            if (_crdTrafoStr == "ETRF2000") {
                rtcmCrs._anchor = 1; // plate-fixed CRS
                rtcmCrs._plateNumber = 7; // Eurasia
                rtcmCrs._databaseLinks << "ISO.DATUM.187" << "ISO.CRS:260" << "ISO.CRS:457"
                    << "EPSG.DATUM:1186" << "EPSG.CRS:7930" << "EPSG.CRS:7931";
            }
            else if (_crdTrafoStr == "DREF91") {
                rtcmCrs._anchor = 1; // plate-fixed CRS
                rtcmCrs._plateNumber = 7; // Eurasia
            }
            else if (_crdTrafoStr == "GDA2020") {
                rtcmCrs._anchor = 1; // plate-fixed CRS
                rtcmCrs._plateNumber = 4; // Australia
                rtcmCrs._databaseLinks << "ISO.DATUM.186" << "ISO.CRS:404" << "ISO.CRS:329"
                    << "EPSG.DATUM:1168" << "EPSG.CRS:7842" << "EPSG.CRS:7843";
            }
            else if (_crdTrafoStr == "SIRGAS2000") {
                rtcmCrs._anchor = 1; // plate-fixed CRS
                rtcmCrs._plateNumber = 12; // S.America
                rtcmCrs._databaseLinks << "ISO.DATUM:169" << "ISO.CRS:384" << "ISO.CRS:313"
                    << "EPSG.DATUM:6674" << "EPSG.CRS:4988" << "EPSG.CRS:4989";
            }
        }
    }

    struct SsrCorr::CodeBias bias;
    memset(&bias, 0, sizeof(bias));
    bias.EpochTime[CLOCKORBIT_SATGPS] = co.EpochTime[CLOCKORBIT_SATGPS];
    bias.EpochTime[CLOCKORBIT_SATGLONASS] = co.EpochTime[CLOCKORBIT_SATGLONASS];
    bias.EpochTime[CLOCKORBIT_SATGALILEO] = co.EpochTime[CLOCKORBIT_SATGALILEO];
    bias.EpochTime[CLOCKORBIT_SATQZSS] = co.EpochTime[CLOCKORBIT_SATQZSS];
    bias.EpochTime[CLOCKORBIT_SATSBAS] = co.EpochTime[CLOCKORBIT_SATSBAS];
    bias.EpochTime[CLOCKORBIT_SATBDS] = co.EpochTime[CLOCKORBIT_SATBDS];
    bias.SSRIOD = _IOD;
    bias.SSRProviderID = _PID;
    bias.SSRSolutionID = _SID;

    struct SsrCorr::PhaseBias phasebias;
    memset(&phasebias, 0, sizeof(phasebias));
    unsigned int dispersiveBiasConsistenyIndicator = 0;
    unsigned int mwConsistencyIndicator = 0;
    phasebias.EpochTime[CLOCKORBIT_SATGPS] = co.EpochTime[CLOCKORBIT_SATGPS];
    phasebias.EpochTime[CLOCKORBIT_SATGLONASS] = co.EpochTime[CLOCKORBIT_SATGLONASS];
    phasebias.EpochTime[CLOCKORBIT_SATGALILEO] = co.EpochTime[CLOCKORBIT_SATGALILEO];
    phasebias.EpochTime[CLOCKORBIT_SATQZSS] = co.EpochTime[CLOCKORBIT_SATQZSS];
    phasebias.EpochTime[CLOCKORBIT_SATSBAS] = co.EpochTime[CLOCKORBIT_SATSBAS];
    phasebias.EpochTime[CLOCKORBIT_SATBDS] = co.EpochTime[CLOCKORBIT_SATBDS];
    phasebias.SSRIOD = _IOD;
    phasebias.SSRProviderID = _PID;
    phasebias.SSRSolutionID = _SID;

    struct SsrCorr::VTEC vtec;
    memset(&vtec, 0, sizeof(vtec));
    vtec.EpochTime = static_cast<int>(epoTime.gpssec());
    vtec.SSRIOD = _IOD;
    vtec.SSRProviderID = _PID;
    vtec.SSRSolutionID = _SID;

    // Update Interval
    // ---------------

    if (_samplRtcmEphCorr == 0.0) {// combined orb and clock
        _samplRtcmEphCorr = _samplRtcmClkCorr = 5.0;
    }
    int clkUpdInd = determineUpdateInd(_samplRtcmClkCorr);
    int ephUpdInd = determineUpdateInd(_samplRtcmEphCorr);

    co.UpdateInterval = clkUpdInd;
    bias.UpdateInterval = ephUpdInd;
    phasebias.UpdateInterval = ephUpdInd;

    for (int ii = 1; ii < lines.size(); ii++) {
        QString key;  // prn or key VTEC, IND (phase bias indicators)
        double rtnUra = 0.0; // [m]
        ColumnVector rtnAPC; rtnAPC.ReSize(3); rtnAPC = 0.0;          // [m, m, m]
        ColumnVector rtnVel; rtnVel.ReSize(3); rtnVel = 0.0;          // [m/s, m/s, m/s]
        ColumnVector rtnCoM; rtnCoM.ReSize(3); rtnCoM = 0.0;          // [m, m, m]
        ColumnVector rtnClk; rtnClk.ReSize(3); rtnClk = 0.0;          // [m, m/s, m/s²]
        ColumnVector rtnClkSig; rtnClkSig.ReSize(3); rtnClkSig = 0.0; // [m, m/s, m/s²]

        //QTextStream in(lines[ii].toLatin1());
        QTextStream in(&lines[ii], QIODevice::ReadOnly);
        in >> key;

        // non-satellite specific parameters
        if (key.contains("IND", Qt::CaseSensitive)) {
            in >> dispersiveBiasConsistenyIndicator >> mwConsistencyIndicator;
            continue;
        }
        // non-satellite specific parameters
        if (key.contains("VTEC", Qt::CaseSensitive)) {
            double ui;
            in >> ui >> vtec.NumLayers;
            vtec.UpdateInterval = (unsigned int)determineUpdateInd(ui);
            for (unsigned ll = 0; ll < vtec.NumLayers; ll++) {
                int dummy;
                in >> dummy >> vtec.Layers[ll].Degree >> vtec.Layers[ll].Order
                    >> vtec.Layers[ll].Height;
                for (unsigned iDeg = 0; iDeg <= vtec.Layers[ll].Degree; iDeg++) {
                    for (unsigned iOrd = 0; iOrd <= vtec.Layers[ll].Order; iOrd++) {
                        in >> vtec.Layers[ll].Cosinus[iDeg][iOrd];
                    }
                }
                for (unsigned iDeg = 0; iDeg <= vtec.Layers[ll].Degree; iDeg++) {
                    for (unsigned iOrd = 0; iOrd <= vtec.Layers[ll].Order; iOrd++) {
                        in >> vtec.Layers[ll].Sinus[iDeg][iOrd];
                    }
                }
            }
            continue;
        }
        // satellite specific parameters
        t_prn prn;
        char sys = key.mid(0, 1).at(0).toLatin1();
        int  num = key.mid(1, 2).toInt();
        int flag = t_corrSSR::getSsrNavTypeFlag(sys, num);
        if (!num) {
            continue;
        }
        prn.set(sys, num, flag);
        QString prnInternalStr = QString::fromStdString(prn.toInternalString());
        QString prnStr = QString::fromStdString(prn.toString());

        const t_eph* ephLast = _ephUser->ephLast(prnInternalStr);
        const t_eph* ephPrev = _ephUser->ephPrev(prnInternalStr);
        const t_eph* eph = ephLast;
        if (eph) {

            // Use previous ephemeris if the last one is too recent
            // ----------------------------------------------------
            const int MINAGE = 60; // seconds
            if (ephPrev && eph->receptDateTime().isValid() &&
                eph->receptDateTime().secsTo(currentDateAndTimeGPS()) < MINAGE) {
                eph = ephPrev;
            }

            // Make sure the clock messages refer to same IOD as orbit messages
            // ----------------------------------------------------------------
            if (_usedEph) {
                if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
                    (*_usedEph)[prnInternalStr] = eph;
                }
                else {
                    eph = 0;
                    if (_usedEph->contains(prnInternalStr)) {
                        const t_eph* usedEph = _usedEph->value(prnInternalStr);
                        if (usedEph == ephLast) {
                            eph = ephLast;
                        }
                        else if (usedEph == ephPrev) {
                            eph = ephPrev;
                        }
                    }
                }
            }
        }

        QDateTime now = currentDateAndTimeGPS();
        bncTime   currentTime(now.toString(Qt::ISODate).toStdString());
        if (eph &&
            !outDatedBcep(eph, currentTime) &&  // detected from storage because of no update
            eph->checkState() != t_eph::bad &&
            eph->checkState() != t_eph::unhealthy &&
            eph->checkState() != t_eph::outdated) {   // detected during reception (bncephuser)
            QMap<QString, double> codeBiases;
            QList<phaseBiasSignal> phaseBiasList;
            phaseBiasesSat pbSat;
            _phaseBiasInformationDecoded = false;

            while (true) {
                QString key;
                int numVal = 0;
                in >> key;
                if (in.status() != QTextStream::Ok) {
                    break;
                }
                if (key == "APC") {
                    in >> numVal;
                    rtnAPC.ReSize(3); rtnAPC = 0.0;
                    for (int ii = 0; ii < numVal; ii++) {
                        in >> rtnAPC[ii];
                    }
                }
                else if (key == "Ura") {
                    in >> numVal;
                    if (numVal == 1)
                        in >> rtnUra;
                }
                else if (key == "Clk") {
                    in >> numVal;
                    rtnClk.ReSize(3); rtnClk = 0.0;
                    for (int ii = 0; ii < numVal; ii++) {
                        in >> rtnClk[ii];
                    }
                }
                else if (key == "ClkSig") {
                    in >> numVal;
                    rtnClkSig.ReSize(3); rtnClkSig = 0.0;
                    for (int ii = 0; ii < numVal; ii++) {
                        in >> rtnClkSig[ii];
                    }
                }
                else if (key == "Vel") {
                    in >> numVal;
                    rtnVel.ReSize(3); rtnVel = 0.0;
                    for (int ii = 0; ii < numVal; ii++) {
                        in >> rtnVel[ii];
                    }
                }
                else if (key == "CoM") {
                    in >> numVal;
                    rtnCoM.ReSize(3); rtnCoM = 0.0;
                    for (int ii = 0; ii < numVal; ii++) {
                        in >> rtnCoM[ii];
                    }
                }
                else if (key == "CodeBias") {
                    in >> numVal;
                    for (int ii = 0; ii < numVal; ii++) {
                        QString type;
                        double value;
                        in >> type >> value;
                        codeBiases[type] = value;
                    }
                }
                else if (key == "YawAngle") {
                    _phaseBiasInformationDecoded = true;
                    in >> numVal >> pbSat.yawAngle;
                    if (pbSat.yawAngle < 0.0) {
                        pbSat.yawAngle += (2 * M_PI);
                    }
                    else if (pbSat.yawAngle > 2 * M_PI) {
                        pbSat.yawAngle -= (2 * M_PI);
                    }
                }
                else if (key == "YawRate") {
                    _phaseBiasInformationDecoded = true;
                    in >> numVal >> pbSat.yawRate;
                }
                else if (key == "PhaseBias") {
                    _phaseBiasInformationDecoded = true;
                    in >> numVal;
                    for (int ii = 0; ii < numVal; ii++) {
                        phaseBiasSignal pb;
                        in >> pb.type >> pb.bias >> pb.integerIndicator
                            >> pb.wlIndicator >> pb.discontinuityCounter;
                        phaseBiasList.append(pb);
                    }
                }
                else {
                    in >> numVal;
                    for (int ii = 0; ii < numVal; ii++) {
                        double dummy;
                        in >> dummy;
                    }
                    emit(newMessage("                      RTNET format error: "
                        + lines[ii].toLatin1(), false));
                    break;
                }
            }

            struct SsrCorr::ClockOrbit::SatData* sd = 0;
            if (prn.system() == 'G') {
                sd = co.Sat + co.NumberOfSat[CLOCKORBIT_SATGPS];
                ++co.NumberOfSat[CLOCKORBIT_SATGPS];
            }
            else if (prn.system() == 'R') {
                sd = co.Sat + CLOCKORBIT_NUMGPS + co.NumberOfSat[CLOCKORBIT_SATGLONASS];
                ++co.NumberOfSat[CLOCKORBIT_SATGLONASS];
            }
            else if (prn.system() == 'E') {
                sd = co.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
                    + co.NumberOfSat[CLOCKORBIT_SATGALILEO];
                ++co.NumberOfSat[CLOCKORBIT_SATGALILEO];
            }
            else if (prn.system() == 'J') {
                sd = co.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
                    + CLOCKORBIT_NUMGALILEO
                    + co.NumberOfSat[CLOCKORBIT_SATQZSS];
                ++co.NumberOfSat[CLOCKORBIT_SATQZSS];
            }
            else if (prn.system() == 'S') {
                sd = co.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
                    + CLOCKORBIT_NUMGALILEO + CLOCKORBIT_NUMQZSS
                    + co.NumberOfSat[CLOCKORBIT_SATSBAS];
                ++co.NumberOfSat[CLOCKORBIT_SATSBAS];
            }
            else if (prn.system() == 'C') {
                sd = co.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
                    + CLOCKORBIT_NUMGALILEO + CLOCKORBIT_NUMQZSS
                    + CLOCKORBIT_NUMSBAS
                    + co.NumberOfSat[CLOCKORBIT_SATBDS];
                ++co.NumberOfSat[CLOCKORBIT_SATBDS];
            }
            if (sd) {
                QString outLine;
                t_irc irc = processSatellite(eph, epoTime.gpsw(), epoTime.gpssec(), prnStr, rtnAPC,
                    rtnUra, rtnClk, rtnVel, rtnCoM, rtnClkSig, sd, outLine);
                if (irc != success) {
                    continue;
                }
            }

            // Code Biases
            // -----------
            struct SsrCorr::CodeBias::BiasSat* biasSat = 0;
            if (!codeBiases.isEmpty()) {
                if (prn.system() == 'G') {
                    biasSat = bias.Sat + bias.NumberOfSat[CLOCKORBIT_SATGPS];
                    ++bias.NumberOfSat[CLOCKORBIT_SATGPS];
                }
                else if (prn.system() == 'R') {
                    biasSat = bias.Sat + CLOCKORBIT_NUMGPS
                        + bias.NumberOfSat[CLOCKORBIT_SATGLONASS];
                    ++bias.NumberOfSat[CLOCKORBIT_SATGLONASS];
                }
                else if (prn.system() == 'E') {
                    biasSat = bias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
                        + bias.NumberOfSat[CLOCKORBIT_SATGALILEO];
                    ++bias.NumberOfSat[CLOCKORBIT_SATGALILEO];
                }
                else if (prn.system() == 'J') {
                    biasSat = bias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
                        + CLOCKORBIT_NUMGALILEO
                        + bias.NumberOfSat[CLOCKORBIT_SATQZSS];
                    ++bias.NumberOfSat[CLOCKORBIT_SATQZSS];
                }
                else if (prn.system() == 'S') {
                    biasSat = bias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
                        + CLOCKORBIT_NUMGALILEO + CLOCKORBIT_NUMQZSS
                        + bias.NumberOfSat[CLOCKORBIT_SATSBAS];
                    ++bias.NumberOfSat[CLOCKORBIT_SATSBAS];
                }
                else if (prn.system() == 'C') {
                    biasSat = bias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
                        + CLOCKORBIT_NUMGALILEO + CLOCKORBIT_NUMQZSS
                        + CLOCKORBIT_NUMSBAS
                        + bias.NumberOfSat[CLOCKORBIT_SATBDS];
                    ++bias.NumberOfSat[CLOCKORBIT_SATBDS];
                }
            }

            if (biasSat) {
                biasSat->ID = prn.number();
                biasSat->NumberOfCodeBiases = 0;
                QMapIterator<QString, double> it(codeBiases);
                while (it.hasNext()) {
                    it.next();
                    int ii = biasSat->NumberOfCodeBiases;
                    if (ii >= CLOCKORBIT_NUMBIAS)
                        break;
                    SsrCorr::CodeType type = _ssrCorr->rnxTypeToCodeType(prn.system(), it.key().toStdString());
                    if (type != _ssrCorr->CODETYPE_RESERVED) {
                        biasSat->NumberOfCodeBiases += 1;
                        biasSat->Biases[ii].Type = type;
                        biasSat->Biases[ii].Bias = it.value();
                        if (_bsx) {
                            QString obsCode = 'C' + it.key();
                            _bsx->write(epoTime.gpsw(), epoTime.gpssec(), prnStr, obsCode, it.value());
                        }
                    }
                }
            }

            // Phase Biases
            // ------------
            struct SsrCorr::PhaseBias::PhaseBiasSat* phasebiasSat = 0;
            if (prn.system() == 'G') {
                phasebiasSat = phasebias.Sat
                    + phasebias.NumberOfSat[CLOCKORBIT_SATGPS];
                ++phasebias.NumberOfSat[CLOCKORBIT_SATGPS];
            }
            else if (prn.system() == 'R') {
                phasebiasSat = phasebias.Sat + CLOCKORBIT_NUMGPS
                    + phasebias.NumberOfSat[CLOCKORBIT_SATGLONASS];
                ++phasebias.NumberOfSat[CLOCKORBIT_SATGLONASS];
            }
            else if (prn.system() == 'E') {
                phasebiasSat = phasebias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
                    + phasebias.NumberOfSat[CLOCKORBIT_SATGALILEO];
                ++phasebias.NumberOfSat[CLOCKORBIT_SATGALILEO];
            }
            else if (prn.system() == 'J') {
                phasebiasSat = phasebias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
                    + CLOCKORBIT_NUMGALILEO
                    + phasebias.NumberOfSat[CLOCKORBIT_SATQZSS];
                ++phasebias.NumberOfSat[CLOCKORBIT_SATQZSS];
            }
            else if (prn.system() == 'S') {
                phasebiasSat = phasebias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
                    + CLOCKORBIT_NUMGALILEO + CLOCKORBIT_NUMQZSS
                    + phasebias.NumberOfSat[CLOCKORBIT_SATSBAS];
                ++phasebias.NumberOfSat[CLOCKORBIT_SATSBAS];
            }
            else if (prn.system() == 'C') {
                phasebiasSat = phasebias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
                    + CLOCKORBIT_NUMGALILEO + CLOCKORBIT_NUMQZSS
                    + CLOCKORBIT_NUMSBAS
                    + phasebias.NumberOfSat[CLOCKORBIT_SATBDS];
                ++phasebias.NumberOfSat[CLOCKORBIT_SATBDS];
            }

            if (phasebiasSat && _phaseBiasInformationDecoded) {
                phasebias.DispersiveBiasConsistencyIndicator = dispersiveBiasConsistenyIndicator;
                phasebias.MWConsistencyIndicator = mwConsistencyIndicator;
                phasebiasSat->ID = prn.number();
                phasebiasSat->NumberOfPhaseBiases = 0;
                phasebiasSat->YawAngle = pbSat.yawAngle;
                phasebiasSat->YawRate = pbSat.yawRate;
                QListIterator<phaseBiasSignal> it(phaseBiasList);
                while (it.hasNext()) {
                    const phaseBiasSignal& pbSig = it.next();
                    int ii = phasebiasSat->NumberOfPhaseBiases;
                    if (ii >= CLOCKORBIT_NUMBIAS)
                        break;
                    SsrCorr::CodeType type = _ssrCorr->rnxTypeToCodeType(prn.system(), pbSig.type.toStdString());
                    if (type != _ssrCorr->PBEXTTYPE_RESERVED) {
                        phasebiasSat->NumberOfPhaseBiases += 1;
                        phasebiasSat->Biases[ii].Type = type;
                        phasebiasSat->Biases[ii].Bias = pbSig.bias;
                        phasebiasSat->Biases[ii].SignalIntegerIndicator = pbSig.integerIndicator;
                        phasebiasSat->Biases[ii].SignalsWideLaneIntegerIndicator = pbSig.wlIndicator;
                        phasebiasSat->Biases[ii].SignalDiscontinuityCounter = pbSig.discontinuityCounter;
                        if (_bsx) {
                            QString obsCode = 'L' + pbSig.type;
                            _bsx->write(epoTime.gpsw(), epoTime.gpssec(), prnStr, obsCode, pbSig.bias);
                        }
                    }
                }
            }
        }
    }

    QByteArray hlpBufferCo;
    char obuffer[CLOCKORBIT_BUFFERSIZE];
    size_t len = 0;

    // Orbit and Clock Corrections together
    // ------------------------------------
    if (_samplRtcmEphCorr == _samplRtcmClkCorr) {
        if (co.NumberOfSat[CLOCKORBIT_SATGPS] > 0
            || co.NumberOfSat[CLOCKORBIT_SATGLONASS] > 0
            || co.NumberOfSat[CLOCKORBIT_SATGALILEO] > 0
            || co.NumberOfSat[CLOCKORBIT_SATBDS] > 0
            || co.NumberOfSat[CLOCKORBIT_SATQZSS] > 0
            || co.NumberOfSat[CLOCKORBIT_SATSBAS] > 0) {
            if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
                memset(obuffer, 0, sizeof(obuffer));
                len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_AUTO, 0, obuffer, sizeof(obuffer));
                if (len > 0) {
                    hlpBufferCo = QByteArray(obuffer, int(len));
                }
            }
        }
    }

    // Orbit and Clock Corrections separately
    // --------------------------------------
    else {
        if (co.NumberOfSat[CLOCKORBIT_SATGPS] > 0) {
            if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
                co.UpdateInterval = ephUpdInd;
                memset(obuffer, 0, sizeof(obuffer));
                len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_GPSORBIT, 1, obuffer, sizeof(obuffer));
                if (len > 0) {
                    hlpBufferCo += QByteArray(obuffer, int(len));
                }
            }
            int mmsg = (co.NumberOfSat[CLOCKORBIT_SATGLONASS] > 0 ||
                co.NumberOfSat[CLOCKORBIT_SATGALILEO] > 0 ||
                co.NumberOfSat[CLOCKORBIT_SATBDS] > 0 ||
                co.NumberOfSat[CLOCKORBIT_SATQZSS] > 0 ||
                co.NumberOfSat[CLOCKORBIT_SATSBAS] > 0) ? 1 : 0;
            if (fmod(epoTime.gpssec(), _samplRtcmClkCorr) == 0.0) {
                co.UpdateInterval = clkUpdInd;
                memset(obuffer, 0, sizeof(obuffer));
                len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_GPSCLOCK, mmsg, obuffer, sizeof(obuffer));
                if (len > 0) {
                    hlpBufferCo += QByteArray(obuffer, int(len));
                }
            }
        }
        if (co.NumberOfSat[CLOCKORBIT_SATGLONASS] > 0) {
            if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
                co.UpdateInterval = ephUpdInd;
                memset(obuffer, 0, sizeof(obuffer));
                len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_GLONASSORBIT, 1, obuffer, sizeof(obuffer));
                if (len > 0) {
                    hlpBufferCo += QByteArray(obuffer, int(len));
                }
            }
            int mmsg = (co.NumberOfSat[CLOCKORBIT_SATGALILEO] > 0 ||
                co.NumberOfSat[CLOCKORBIT_SATBDS] > 0 ||
                co.NumberOfSat[CLOCKORBIT_SATQZSS] > 0 ||
                co.NumberOfSat[CLOCKORBIT_SATSBAS] > 0) ? 1 : 0;
            if (fmod(epoTime.gpssec(), _samplRtcmClkCorr) == 0.0) {
                co.UpdateInterval = clkUpdInd;
                memset(obuffer, 0, sizeof(obuffer));
                len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_GLONASSCLOCK, mmsg, obuffer, sizeof(obuffer));
                if (len > 0) {
                    hlpBufferCo += QByteArray(obuffer, int(len));
                }
            }
        }
        if (co.NumberOfSat[CLOCKORBIT_SATGALILEO] > 0) {
            if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
                co.UpdateInterval = ephUpdInd;
                memset(obuffer, 0, sizeof(obuffer));
                len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_GALILEOORBIT, 1, obuffer, sizeof(obuffer));
                if (len > 0) {
                    hlpBufferCo += QByteArray(obuffer, int(len));
                }
            }
            int mmsg = (co.NumberOfSat[CLOCKORBIT_SATBDS] > 0 ||
                co.NumberOfSat[CLOCKORBIT_SATQZSS] > 0 ||
                co.NumberOfSat[CLOCKORBIT_SATSBAS] > 0) ? 1 : 0;
            if (fmod(epoTime.gpssec(), _samplRtcmClkCorr) == 0.0) {
                co.UpdateInterval = clkUpdInd;
                memset(obuffer, 0, sizeof(obuffer));
                len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_GALILEOCLOCK, mmsg, obuffer, sizeof(obuffer));
                if (len > 0) {
                    hlpBufferCo += QByteArray(obuffer, int(len));
                }
            }
        }
        if (co.NumberOfSat[CLOCKORBIT_SATBDS] > 0) {
            if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
                co.UpdateInterval = ephUpdInd;
                memset(obuffer, 0, sizeof(obuffer));
                len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_BDSORBIT, 1, obuffer, sizeof(obuffer));
                if (len > 0) {
                    hlpBufferCo += QByteArray(obuffer, int(len));
                }
            }
            int mmsg = (co.NumberOfSat[CLOCKORBIT_SATQZSS] > 0 ||
                co.NumberOfSat[CLOCKORBIT_SATSBAS] > 0) ? 1 : 0;
            if (fmod(epoTime.gpssec(), _samplRtcmClkCorr) == 0.0) {
                co.UpdateInterval = clkUpdInd;
                memset(obuffer, 0, sizeof(obuffer));
                len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_BDSCLOCK, mmsg, obuffer, sizeof(obuffer));
                if (len > 0) {
                    hlpBufferCo += QByteArray(obuffer, int(len));
                }
            }
        }
        if (co.NumberOfSat[CLOCKORBIT_SATQZSS] > 0) {
            if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
                co.UpdateInterval = ephUpdInd;
                memset(obuffer, 0, sizeof(obuffer));
                len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_QZSSORBIT, 1, obuffer, sizeof(obuffer));
                if (len > 0) {
                    hlpBufferCo += QByteArray(obuffer, int(len));
                }
            }
            int mmsg = (co.NumberOfSat[CLOCKORBIT_SATSBAS] > 0) ? 1 : 0;
            if (fmod(epoTime.gpssec(), _samplRtcmClkCorr) == 0.0) {
                co.UpdateInterval = clkUpdInd;
                memset(obuffer, 0, sizeof(obuffer));
                len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_QZSSCLOCK, mmsg, obuffer, sizeof(obuffer));
                if (len > 0) {
                    hlpBufferCo += QByteArray(obuffer, int(len));
                }
            }
        }
        if (co.NumberOfSat[CLOCKORBIT_SATSBAS] > 0) {
            if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
                co.UpdateInterval = ephUpdInd;
                memset(obuffer, 0, sizeof(obuffer));
                len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_SBASORBIT, 1, obuffer, sizeof(obuffer));
                co.UpdateInterval = clkUpdInd;
                if (len > 0) {
                    hlpBufferCo += QByteArray(obuffer, int(len));
                }
            }
            int mmsg = 0;
            if (fmod(epoTime.gpssec(), _samplRtcmClkCorr) == 0.0) {
                co.UpdateInterval = clkUpdInd;
                memset(obuffer, 0, sizeof(obuffer));
                len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_SBASCLOCK, mmsg, obuffer, sizeof(obuffer));
                if (len > 0) {
                    hlpBufferCo += QByteArray(obuffer, int(len));
                }
            }
        }
    }

    // Code Biases
    // -----------
    QByteArray hlpBufferBias;
    if (bias.NumberOfSat[CLOCKORBIT_SATGPS] > 0
        || bias.NumberOfSat[CLOCKORBIT_SATGLONASS] > 0
        || bias.NumberOfSat[CLOCKORBIT_SATGALILEO] > 0
        || bias.NumberOfSat[CLOCKORBIT_SATBDS] > 0
        || bias.NumberOfSat[CLOCKORBIT_SATQZSS] > 0
        || bias.NumberOfSat[CLOCKORBIT_SATSBAS] > 0) {
        if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
            memset(obuffer, 0, sizeof(obuffer));
            len = _ssrCorr->MakeCodeBias(&bias, _ssrCorr->CBTYPE_AUTO, 0, obuffer, sizeof(obuffer));
            if (len > 0) {
                hlpBufferBias = QByteArray(obuffer, int(len));
            }
        }
    }

    // Phase Biases
    // ------------
    QByteArray hlpBufferPhaseBias;
    if ((phasebias.NumberOfSat[CLOCKORBIT_SATGPS] > 0
        || phasebias.NumberOfSat[CLOCKORBIT_SATGLONASS] > 0
        || phasebias.NumberOfSat[CLOCKORBIT_SATGALILEO] > 0
        || phasebias.NumberOfSat[CLOCKORBIT_SATBDS] > 0
        || phasebias.NumberOfSat[CLOCKORBIT_SATQZSS] > 0
        || phasebias.NumberOfSat[CLOCKORBIT_SATSBAS] > 0) && (_phaseBiasInformationDecoded)) {
        if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
            memset(obuffer, 0, sizeof(obuffer));
            len = _ssrCorr->MakePhaseBias(&phasebias, _ssrCorr->PBTYPE_AUTO, 0, obuffer, sizeof(obuffer));
            if (len > 0) {
                hlpBufferPhaseBias = QByteArray(obuffer, int(len));
            }
        }
    }

    // VTEC
    // ----
    QByteArray hlpBufferVtec;
    if (vtec.NumLayers > 0) {
        if (fmod(epoTime.gpssec(), _samplRtcmVtec) == 0.0) {
            memset(obuffer, 0, sizeof(obuffer));
            len = _ssrCorr->MakeVTEC(&vtec, 0, obuffer, sizeof(obuffer));
            if (len > 0) {
                hlpBufferVtec = QByteArray(obuffer, int(len));
            }
        }
    }

    // Service CRS
    // -----------
    QByteArray hlpBufferServiceCrs;
    if (sizeof(serviceCrs._name) > 0) {
        if (fmod(epoTime.gpssec(), _samplRtcmCrs) == 0.0) {
            memset(obuffer, 0, sizeof(obuffer));
            len = t_crsEncoder::RTCM3(serviceCrs, obuffer, sizeof(obuffer));
            if (len > 0) {
                hlpBufferServiceCrs = QByteArray(obuffer, int(len));
            }
        }
    }

    // RTCM CRS
    // --------
    QByteArray hlpBufferRtcmCrs;
    if (sizeof(rtcmCrs._name) > 0) {
        if (fmod(epoTime.gpssec(), _samplRtcmCrs) == 0.0) {
            memset(obuffer, 0, sizeof(obuffer));
            len = t_crsEncoder::RTCM3(rtcmCrs, obuffer, sizeof(obuffer));
            if (len > 0) {
                hlpBufferRtcmCrs = QByteArray(obuffer, int(len));
            }
        }
    }

    // Create OutBuffer
    // ----------------
    _outBuffer += hlpBufferCo + hlpBufferBias + hlpBufferPhaseBias + hlpBufferVtec
        + hlpBufferServiceCrs + hlpBufferRtcmCrs + '\0';
}
//
////////////////////////////////////////////////////////////////////////////
t_irc bncRtnetUploadCaster::processSatellite(const t_eph* eph, int GPSweek,
    double GPSweeks, const QString& prn, const ColumnVector& rtnAPC,
    double rtnUra, const ColumnVector& rtnClk, const ColumnVector& rtnVel,
    const ColumnVector& rtnCoM, const ColumnVector& rtnClkSig,
    struct SsrCorr::ClockOrbit::SatData* sd, QString& outLine) {

    // Broadcast Position and Velocity
    // -------------------------------
    ColumnVector xB(6);
    ColumnVector vB(3);
    t_irc irc = eph->getCrd(bncTime(GPSweek, GPSweeks), xB, vB, false);

    if (irc != success) {
        return irc;
    }

    // Precise Position
    // ----------------
    ColumnVector xP = _CoM ? rtnCoM : rtnAPC;

    if (xP.size() == 0) {
        return failure;
    }

    double dc = 0.0;
    if (_crdTrafoStr != "IGS20") {
        crdTrafo14(GPSweek, xP, dc); // ITRF2020 => ITRF2014
        crdTrafo(GPSweek, xP, dc);   // ITRF2014 to other reference frames
    }

    // Difference in xyz
    // -----------------
    ColumnVector dx = xB.Rows(1, 3) - xP;
    ColumnVector dv = vB - rtnVel;

    // Difference in RSW
    // -----------------
    ColumnVector rsw(3);
    XYZ_to_RSW(xB.Rows(1, 3), vB, dx, rsw);

    ColumnVector dotRsw(3);
    XYZ_to_RSW(xB.Rows(1, 3), vB, dv, dotRsw);

    // Clock Correction
    // ----------------
    double dClkA0 = rtnClk(1) - (xB(4) - dc) * t_CST::c;
    double dClkA1 = 0.0;
    if (rtnClk(2)) {
        dClkA1 = rtnClk(2) - xB(5) * t_CST::c;
    }
    double dClkA2 = 0.0;
    if (rtnClk(3)) {
        dClkA2 = rtnClk(3) - xB(6) * t_CST::c;
    }

    if (sd) {
        sd->ID = prn.mid(1).toInt();
        sd->IOD = eph->IOD();
        sd->Clock.DeltaA0 = dClkA0;
        sd->Clock.DeltaA1 = dClkA1;
        sd->Clock.DeltaA2 = dClkA2;
        sd->UserRangeAccuracy = rtnUra;
        sd->Orbit.DeltaRadial = rsw(1);
        sd->Orbit.DeltaAlongTrack = rsw(2);
        sd->Orbit.DeltaCrossTrack = rsw(3);
        sd->Orbit.DotDeltaRadial = dotRsw(1);
        sd->Orbit.DotDeltaAlongTrack = dotRsw(2);
        sd->Orbit.DotDeltaCrossTrack = dotRsw(3);

        if (corrIsOutOfRange(sd)) {
            emit(newMessage(QString("bncRtnetUploadCaster: SSR parameter is out of its defined range").toLatin1(), false));
            return failure;
        }
    }

    outLine = QString().asprintf("%d %.1f %s  %u  %10.3f %8.3f %8.3f  %8.3f %8.3f %8.3f\n", GPSweek,
        GPSweeks, eph->prn().toString().c_str(), eph->IOD(), dClkA0, dClkA1, dClkA2,
        rsw(1), rsw(2), rsw(3));  //fprintf(stderr, "%s\n", outLine.toStdString().c_str());

    // RTNET full clock for RINEX and SP3 file
    // ---------------------------------------
    double relativity = -2.0 * DotProduct(xP, rtnVel) / t_CST::c;
    double clkRnx = (rtnClk[0] - relativity) / t_CST::c;  // [s]
    double clkRnxRate = rtnClk[1] / t_CST::c;                 // [s/s  = -]
    double clkRnxAcc = rtnClk[2] / t_CST::c;                 // [s/s² = -/s]

    if (_rnx) {
        double clkRnxSig, clkRnxRateSig, clkRnxAccSig;
        int s = rtnClkSig.size();
        switch (s) {
        case 1:
            clkRnxSig = rtnClkSig[0] / t_CST::c;    // [s]
            clkRnxRateSig = 0.0;                        // [s/s = -]
            clkRnxAccSig = 0.0;                        // [s/s² ) -/s]
            break;
        case 2:
            clkRnxSig = rtnClkSig[0] / t_CST::c;     // [s]
            clkRnxRateSig = rtnClkSig[1] / t_CST::c;     // [s/s = -]
            clkRnxAccSig = 0.0;                         // [s/s² ) -/s]
            break;
        case 3:
            clkRnxSig = rtnClkSig[0] / t_CST::c;     // [s]
            clkRnxRateSig = rtnClkSig[1] / t_CST::c;     // [s/s = -]
            clkRnxAccSig = rtnClkSig[2] / t_CST::c;     // [s/s² ) -/s]
            break;
        }
        _rnx->write(GPSweek, GPSweeks, prn, clkRnx, clkRnxRate, clkRnxAcc,
            clkRnxSig, clkRnxRateSig, clkRnxAccSig);
    }
    if (_sp3) {
        _sp3->write(GPSweek, GPSweeks, prn, rtnCoM, clkRnx, rtnVel, clkRnxRate);
    }
    return success;
}

// Transform Coordinates
////////////////////////////////////////////////////////////////////////////
void bncRtnetUploadCaster::crdTrafo(int GPSWeek, ColumnVector& xyz,
    double& dc) {

    // Current epoch minus 2000.0 in years
    // ------------------------------------
    double dt = (GPSWeek - (1042.0 + 6.0 / 7.0)) / 365.2422 * 7.0 + 2000.0 - _t0;

    ColumnVector dx(3);

    dx(1) = _dx + dt * _dxr;
    dx(2) = _dy + dt * _dyr;
    dx(3) = _dz + dt * _dzr;

    static const double arcSec = 180.0 * 3600.0 / M_PI;

    double ox = (_ox + dt * _oxr) / arcSec;
    double oy = (_oy + dt * _oyr) / arcSec;
    double oz = (_oz + dt * _ozr) / arcSec;

    double sc = 1.0 + _sc * 1e-9 + dt * _scr * 1e-9;

    // Specify approximate center of area
    // ----------------------------------
    ColumnVector meanSta(3);

    if (_crdTrafoStr == "ETRF2000") {
        meanSta(1) = 3661090.0;
        meanSta(2) = 845230.0;
        meanSta(3) = 5136850.0;
    }
    else if (_crdTrafoStr == "GDA2020") {
        meanSta(1) = -4052050.0;
        meanSta(2) = 4212840.0;
        meanSta(3) = -2545110.0;
    }
    else if (_crdTrafoStr == "SIRGAS2000") {
        meanSta(1) = 3740860.0;
        meanSta(2) = -4964290.0;
        meanSta(3) = -1425420.0;
    }
    else if (_crdTrafoStr == "DREF91") {
        meanSta(1) = 3959579.0;
        meanSta(2) = 721719.0;
        meanSta(3) = 4931539.0;
    }
    else if (_crdTrafoStr == "Custom") {
        meanSta(1) = 0.0;
        meanSta(2) = 0.0;
        meanSta(3) = 0.0;
    }

    // Clock correction proportional to topocentric distance to satellites
    // -------------------------------------------------------------------
    double rho = (xyz - meanSta).NormFrobenius();
    dc = rho * (sc - 1.0) / sc / t_CST::c;

    Matrix rMat(3, 3);
    rMat(1, 1) = 1.0;
    rMat(1, 2) = -oz;
    rMat(1, 3) = oy;
    rMat(2, 1) = oz;
    rMat(2, 2) = 1.0;
    rMat(2, 3) = -ox;
    rMat(3, 1) = -oy;
    rMat(3, 2) = ox;
    rMat(3, 3) = 1.0;

    xyz = sc * rMat * xyz + dx;
}

// Transform Coordinates
////////////////////////////////////////////////////////////////////////////
void bncRtnetUploadCaster::crdTrafo14(int GPSWeek, ColumnVector& xyz,
    double& dc) {

    // Current epoch minus 2000.0 in years
    // ------------------------------------
    double dt = (GPSWeek - (1042.0 + 6.0 / 7.0)) / 365.2422 * 7.0 + 2000.0 - _t0;

    ColumnVector dx(3);

    dx(1) = _dx14 + dt * _dxr14;
    dx(2) = _dy14 + dt * _dyr14;
    dx(3) = _dz14 + dt * _dzr14;

    static const double arcSec = 180.0 * 3600.0 / M_PI;

    double ox = (_ox14 + dt * _oxr14) / arcSec;
    double oy = (_oy14 + dt * _oyr14) / arcSec;
    double oz = (_oz14 + dt * _ozr14) / arcSec;

    double sc = 1.0 + _sc14 * 1e-9 + dt * _scr14 * 1e-9;

    // Specify approximate center of area
    // ----------------------------------
    ColumnVector meanSta(3);
    meanSta(1) = 0.0; // TODO
    meanSta(2) = 0.0; // TODO
    meanSta(3) = 0.0; // TODO

    // Clock correction proportional to topocentric distance to satellites
    // -------------------------------------------------------------------
    double rho = (xyz - meanSta).NormFrobenius();
    dc = rho * (sc - 1.0) / sc / t_CST::c;

    Matrix rMat(3, 3);
    rMat(1, 1) = 1.0;
    rMat(1, 2) = -oz;
    rMat(1, 3) = oy;
    rMat(2, 1) = oz;
    rMat(2, 2) = 1.0;
    rMat(2, 3) = -ox;
    rMat(3, 1) = -oy;
    rMat(3, 2) = ox;
    rMat(3, 3) = 1.0;

    xyz = sc * rMat * xyz + dx;
}

// Update Interval
////////////////////////////////////////////////////////////////////////////
int bncRtnetUploadCaster::determineUpdateInd(double samplingRate) {

    if (samplingRate == 1.0) {
        return 0;
    }
    else if (samplingRate == 2.0) {
        return 1;
    }
    else if (samplingRate == 5.0) {
        return 2;
    }
    else if (samplingRate == 10.0) {
        return 3;
    }
    else if (samplingRate == 15.0) {
        return 4;
    }
    else if (samplingRate == 30.0) {
        return 5;
    }
    else if (samplingRate == 60.0) {
        return 6;
    }
    else if (samplingRate == 120.0) {
        return 7;
    }
    else if (samplingRate == 240.0) {
        return 8;
    }
    else if (samplingRate == 300.0) {
        return 9;
    }
    else if (samplingRate == 600.0) {
        return 10;
    }
    else if (samplingRate == 900.0) {
        return 11;
    }
    else if (samplingRate == 1800.0) {
        return 12;
    }
    else if (samplingRate == 3600.0) {
        return 13;
    }
    else if (samplingRate == 7200.0) {
        return 14;
    }
    else if (samplingRate == 10800.0) {
        return 15;
    }
    return 2;  // default
}

// Check corrections
////////////////////////////////////////////////////////////////////////////
bool bncRtnetUploadCaster::corrIsOutOfRange(struct SsrCorr::ClockOrbit::SatData* sd) {

    if (fabs(sd->Clock.DeltaA0) > 209.7151) { return true; }
    if (fabs(sd->Clock.DeltaA1) > 1.048575) { return true; }
    if (fabs(sd->Clock.DeltaA2) > 1.34217726) { return true; }

    if (fabs(sd->Orbit.DeltaRadial) > 209.7151) { return true; }
    if (fabs(sd->Orbit.DeltaAlongTrack) > 209.7148) { return true; }
    if (fabs(sd->Orbit.DeltaCrossTrack) > 209.7148) { return true; }

    if (fabs(sd->Orbit.DotDeltaRadial) > 1.048575) { return true; }
    if (fabs(sd->Orbit.DotDeltaAlongTrack) > 1.048572) { return true; }
    if (fabs(sd->Orbit.DotDeltaCrossTrack) > 1.048572) { return true; }
    return false;
}
