| 1 | // Part of BNC, a utility for retrieving decoding and
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| 2 | // converting GNSS data streams from NTRIP broadcasters.
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| 3 | //
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| 4 | // Copyright (C) 2007
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| 5 | // German Federal Agency for Cartography and Geodesy (BKG)
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| 6 | // http://www.bkg.bund.de
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| 7 | // Czech Technical University Prague, Department of Geodesy
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| 8 | // http://www.fsv.cvut.cz
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| 9 | //
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| 10 | // Email: euref-ip@bkg.bund.de
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| 11 | //
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| 12 | // This program is free software; you can redistribute it and/or
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| 13 | // modify it under the terms of the GNU General Public License
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| 14 | // as published by the Free Software Foundation, version 2.
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| 15 | //
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| 16 | // This program is distributed in the hope that it will be useful,
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| 17 | // but WITHOUT ANY WARRANTY; without even the implied warranty of
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| 18 | // MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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| 19 | // GNU General Public License for more details.
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| 20 | //
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| 21 | // You should have received a copy of the GNU General Public License
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| 22 | // along with this program; if not, write to the Free Software
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| 23 | // Foundation, Inc., 59 Temple Place - Suite 330, Boston, MA 02111-1307, USA.
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| 24 |
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| 25 | /* -------------------------------------------------------------------------
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| 26 | * BKG NTRIP Client
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| 27 | * -------------------------------------------------------------------------
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| 28 | *
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| 29 | * Class: RTCM3coDecoder
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| 30 | *
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| 31 | * Purpose: RTCM3 Clock Orbit Decoder
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| 32 | *
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| 33 | * Author: L. Mervart
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| 34 | *
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| 35 | * Created: 05-May-2008
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| 36 | *
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| 37 | * Changes:
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| 38 | *
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| 39 | * -----------------------------------------------------------------------*/
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| 40 |
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| 41 | #include <stdio.h>
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| 42 | #include <math.h>
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| 43 |
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| 44 | #include "RTCM3coDecoder.h"
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| 45 | #include "bncutils.h"
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| 46 | #include "bncrinex.h"
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| 47 | #include "bncapp.h"
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| 48 | #include "bncsettings.h"
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| 49 | #include "rtcm3torinex.h"
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| 50 |
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| 51 | using namespace std;
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| 52 |
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| 53 | // Constructor
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| 54 | ////////////////////////////////////////////////////////////////////////////
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| 55 | RTCM3coDecoder::RTCM3coDecoder(const QString& staID) {
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| 56 |
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| 57 | _staID = staID;
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| 58 |
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| 59 | // File Output
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| 60 | // -----------
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| 61 | bncSettings settings;
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| 62 | QString path = settings.value("corrPath").toString();
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| 63 | if (!path.isEmpty()) {
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| 64 | expandEnvVar(path);
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| 65 | if ( path.length() > 0 && path[path.length()-1] != QDir::separator() ) {
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| 66 | path += QDir::separator();
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| 67 | }
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| 68 | _fileNameSkl = path + staID;
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| 69 | }
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| 70 | _out = 0;
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| 71 | _GPSweeks = -1.0;
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| 72 |
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| 73 | connect(this, SIGNAL(newCorrLine(QString, QString, long)),
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| 74 | (bncApp*) qApp, SLOT(slotNewCorrLine(QString, QString, long)));
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| 75 |
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| 76 | memset(&_co, 0, sizeof(_co));
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| 77 | }
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| 78 |
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| 79 | // Destructor
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| 80 | ////////////////////////////////////////////////////////////////////////////
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| 81 | RTCM3coDecoder::~RTCM3coDecoder() {
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| 82 | delete _out;
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| 83 | }
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| 84 |
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| 85 | // Reopen Output File
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| 86 | ////////////////////////////////////////////////////////////////////////
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| 87 | void RTCM3coDecoder::reopen() {
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| 88 |
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| 89 | if (!_fileNameSkl.isEmpty()) {
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| 90 |
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| 91 | bncSettings settings;
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| 92 |
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| 93 | QDateTime datTim = currentDateAndTimeGPS();
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| 94 |
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| 95 | QString hlpStr = bncRinex::nextEpochStr(datTim,
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| 96 | settings.value("corrIntr").toString());
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| 97 |
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| 98 | QString fileName = _fileNameSkl
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| 99 | + QString("%1").arg(datTim.date().dayOfYear(), 3, 10, QChar('0'))
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| 100 | + hlpStr + datTim.toString(".yyC");
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| 101 |
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| 102 | if (_fileName == fileName) {
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| 103 | return;
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| 104 | }
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| 105 | else {
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| 106 | _fileName = fileName;
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| 107 | }
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| 108 |
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| 109 | delete _out;
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| 110 | if ( Qt::CheckState(settings.value("rnxAppend").toInt()) == Qt::Checked) {
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| 111 | _out = new ofstream( _fileName.toAscii().data(),
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| 112 | ios_base::out | ios_base::app );
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| 113 | }
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| 114 | else {
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| 115 | _out = new ofstream( _fileName.toAscii().data() );
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| 116 | }
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| 117 | }
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| 118 | }
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| 119 |
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| 120 | //
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| 121 | ////////////////////////////////////////////////////////////////////////////
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| 122 | t_irc RTCM3coDecoder::Decode(char* buffer, int bufLen, vector<string>& errmsg) {
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| 123 |
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| 124 | errmsg.clear();
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| 125 |
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| 126 | _buffer.append(QByteArray(buffer,bufLen));
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| 127 |
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| 128 | t_irc retCode = failure;
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| 129 |
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| 130 | while(_buffer.size()) {
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| 131 |
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| 132 | int bytesused = 0;
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| 133 | struct ClockOrbit co_sav;
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| 134 | memcpy(&co_sav, &_co, sizeof(co_sav)); // save state
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| 135 |
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| 136 | GCOB_RETURN irc = GetClockOrbitBias(&_co, &_bias, _buffer.data(),
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| 137 | _buffer.size(), &bytesused);
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| 138 |
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| 139 | if (irc <= -30) { // not enough data - restore state and exit loop
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| 140 | memcpy(&_co, &co_sav, sizeof(co_sav));
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| 141 | break;
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| 142 | }
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| 143 |
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| 144 | else if (irc < 0) { // error - skip 1 byte and retry
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| 145 | memset(&_co, 0, sizeof(_co));
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| 146 | memset(&_bias, 0, sizeof(_bias));
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| 147 | _buffer = _buffer.mid(bytesused ? bytesused : 1);
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| 148 | }
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| 149 |
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| 150 | else { // OK or MESSAGEFOLLOWS
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| 151 | _buffer = _buffer.mid(bytesused);
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| 152 |
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| 153 | if (irc == GCOBR_OK) {
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| 154 | reopen();
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| 155 |
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| 156 | // Guess GPS week and sec using system time
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| 157 | // ----------------------------------------
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| 158 | int GPSweek;
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| 159 | double GPSweeksHlp;
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| 160 | currentGPSWeeks(GPSweek, GPSweeksHlp);
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| 161 |
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| 162 | // Correction Epoch from GPSEpochTime
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| 163 | // ----------------------------------
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| 164 | if (_co.NumberOfGPSSat > 0) {
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| 165 | if (GPSweeksHlp > _co.GPSEpochTime + 86400.0) {
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| 166 | GPSweek += 1;
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| 167 | }
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| 168 | else if (GPSweeksHlp < _co.GPSEpochTime - 86400.0) {
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| 169 | GPSweek -= 1;
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| 170 | }
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| 171 | _GPSweeks = _co.GPSEpochTime;
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| 172 | }
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| 173 |
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| 174 | // Correction Epoch from Glonass Epoch
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| 175 | // -----------------------------------
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| 176 | else if (_co.NumberOfGLONASSSat > 0){
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| 177 |
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| 178 | // Second of day (GPS time) from Glonass Epoch
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| 179 | // -------------------------------------------
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| 180 | QDate date = dateAndTimeFromGPSweek(GPSweek, GPSweeksHlp).date();
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| 181 | int leapSecond = gnumleap(date.year(), date.month(), date.day());
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| 182 | int GPSDaySec = _co.GLONASSEpochTime - 3 * 3600 + leapSecond;
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| 183 |
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| 184 | int weekDay = int(GPSweeksHlp/86400.0);
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| 185 | int GPSDaySecHlp = int(GPSweeksHlp) - weekDay * 86400;
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| 186 |
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| 187 | // Handle the difference between system clock and correction epoch
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| 188 | // ---------------------------------------------------------------
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| 189 | if (GPSDaySec < GPSDaySecHlp - 3600) {
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| 190 | weekDay += 1;
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| 191 | if (weekDay > 6) {
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| 192 | weekDay = 0;
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| 193 | GPSweek += 1;
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| 194 | }
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| 195 | }
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| 196 | else if (GPSDaySec > GPSDaySecHlp + 3600) {
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| 197 | weekDay -= 1;
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| 198 | if (weekDay < 0) {
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| 199 | weekDay = 6;
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| 200 | GPSweek -= 1;
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| 201 | }
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| 202 | }
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| 203 |
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| 204 | _GPSweeks = weekDay * 86400.0 + GPSDaySec;
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| 205 | }
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| 206 |
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| 207 | long coTime = GPSweek * 7*24*3600 + long(floor(_GPSweeks+0.5));
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| 208 |
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| 209 | // Loop over all satellites (GPS and Glonass)
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| 210 | // ------------------------------------------
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| 211 | for (int ii = 0; ii < CLOCKORBIT_NUMGPS+_co.NumberOfGLONASSSat; ii++) {
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| 212 | char sysCh = ' ';
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| 213 | if (ii < _co.NumberOfGPSSat) {
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| 214 | sysCh = 'G';
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| 215 | }
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| 216 | else if (ii >= CLOCKORBIT_NUMGPS) {
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| 217 | sysCh = 'R';
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| 218 | }
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| 219 | if (sysCh != ' ') {
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| 220 |
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| 221 | QString linePart;
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| 222 | linePart.sprintf("%d %d %d %.1f %c%2.2d",
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| 223 | _co.messageType, _co.UpdateInterval, GPSweek, _GPSweeks,
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| 224 | sysCh, _co.Sat[ii].ID);
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| 225 |
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| 226 | // Combined message (orbit and clock)
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| 227 | // ----------------------------------
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| 228 | if ( _co.messageType == COTYPE_GPSCOMBINED ||
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| 229 | _co.messageType == COTYPE_GLONASSCOMBINED ) {
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| 230 | QString line;
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| 231 | line.sprintf(" %3d"
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| 232 | " %8.3f %8.3f %8.3f %8.3f"
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| 233 | " %8.3f %8.3f %8.3f %8.3f"
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| 234 | " %8.3f %8.3f %8.3f %8.3f",
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| 235 | _co.Sat[ii].IOD,
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| 236 | _co.Sat[ii].Clock.DeltaA0,
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| 237 | _co.Sat[ii].Orbit.DeltaRadial,
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| 238 | _co.Sat[ii].Orbit.DeltaAlongTrack,
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| 239 | _co.Sat[ii].Orbit.DeltaCrossTrack,
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| 240 | _co.Sat[ii].Clock.DeltaA1,
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| 241 | _co.Sat[ii].Orbit.DotDeltaRadial,
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| 242 | _co.Sat[ii].Orbit.DotDeltaAlongTrack,
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| 243 | _co.Sat[ii].Orbit.DotDeltaCrossTrack,
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| 244 | _co.Sat[ii].Clock.DeltaA2,
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| 245 | _co.Sat[ii].Orbit.DotDotDeltaRadial,
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| 246 | _co.Sat[ii].Orbit.DotDotDeltaAlongTrack,
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| 247 | _co.Sat[ii].Orbit.DotDotDeltaCrossTrack);
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| 248 | printLine(linePart+line, coTime);
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| 249 | }
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| 250 |
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| 251 | // Orbits only
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| 252 | // -----------
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| 253 | else if ( _co.messageType == COTYPE_GPSORBIT ||
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| 254 | _co.messageType == COTYPE_GLONASSORBIT ) {
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| 255 | QString line;
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| 256 | line.sprintf(" %3d"
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| 257 | " %8.3f %8.3f %8.3f"
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| 258 | " %8.3f %8.3f %8.3f"
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| 259 | " %8.3f %8.3f %8.3f",
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| 260 | _co.Sat[ii].IOD,
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| 261 | _co.Sat[ii].Orbit.DeltaRadial,
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| 262 | _co.Sat[ii].Orbit.DeltaAlongTrack,
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| 263 | _co.Sat[ii].Orbit.DeltaCrossTrack,
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| 264 | _co.Sat[ii].Orbit.DotDeltaRadial,
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| 265 | _co.Sat[ii].Orbit.DotDeltaAlongTrack,
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| 266 | _co.Sat[ii].Orbit.DotDeltaCrossTrack,
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| 267 | _co.Sat[ii].Orbit.DotDotDeltaRadial,
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| 268 | _co.Sat[ii].Orbit.DotDotDeltaAlongTrack,
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| 269 | _co.Sat[ii].Orbit.DotDotDeltaCrossTrack);
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| 270 | printLine(linePart+line, coTime);
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| 271 | }
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| 272 |
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| 273 | // Clocks only
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| 274 | // -----------
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| 275 | else if ( _co.messageType == COTYPE_GPSCLOCK ||
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| 276 | _co.messageType == COTYPE_GLONASSCLOCK ) {
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| 277 | QString line;
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| 278 | line.sprintf(" %3d %8.3f %8.3f %8.3f",
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| 279 | _co.Sat[ii].IOD,
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| 280 | _co.Sat[ii].Clock.DeltaA0,
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| 281 | _co.Sat[ii].Clock.DeltaA1,
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| 282 | _co.Sat[ii].Clock.DeltaA2);
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| 283 | printLine(linePart+line, coTime);
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| 284 | }
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| 285 |
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| 286 | // User Range Accuracy
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| 287 | // -------------------
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| 288 | else if ( _co.messageType == COTYPE_GPSURA ||
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| 289 | _co.messageType == COTYPE_GLONASSURA ) {
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| 290 | QString line;
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| 291 | line.sprintf(" %3d %d",
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| 292 | _co.Sat[ii].IOD, _co.Sat[ii].URA);
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| 293 | printLine(linePart+line, coTime);
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| 294 | }
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| 295 |
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| 296 | // High-Resolution Clocks
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| 297 | // ----------------------
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| 298 | else if ( _co.messageType == COTYPE_GPSHR ||
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| 299 | _co.messageType == COTYPE_GLONASSHR ) {
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| 300 | QString line;
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| 301 | line.sprintf(" %3d %8.3f",
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| 302 | _co.Sat[ii].IOD, _co.Sat[ii].hrclock);
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| 303 | printLine(linePart+line, coTime);
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| 304 | }
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| 305 | }
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| 306 | }
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| 307 |
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| 308 | // Loop over all satellites (GPS and Glonass)
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| 309 | // ------------------------------------------
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| 310 | for (int ii = 0; ii < CLOCKORBIT_NUMGPS + _bias.NumberOfGLONASSSat; ii++) {
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| 311 | char sysCh = ' ';
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| 312 | if (ii < _bias.NumberOfGPSSat) {
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| 313 | sysCh = 'G';
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| 314 | }
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| 315 | else if (ii >= CLOCKORBIT_NUMGPS) {
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| 316 | sysCh = 'R';
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| 317 | }
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| 318 | if (sysCh != ' ') {
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| 319 | QString line;
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| 320 | line.sprintf("%d %d %d %.1f %c%2.2d %d",
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| 321 | _bias.messageType, _bias.UpdateInterval, GPSweek, _GPSweeks,
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| 322 | sysCh, _bias.Sat[ii].ID,
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| 323 | _bias.Sat[ii].NumberOfCodeBiases);
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| 324 | for (int jj = 0; jj < _bias.Sat[ii].NumberOfCodeBiases; jj++) {
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| 325 | QString hlp;
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| 326 | hlp.sprintf(" %d %8.3f", _bias.Sat[ii].Biases[jj].Type,
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| 327 | _bias.Sat[ii].Biases[jj].Bias);
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| 328 | line += hlp;
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| 329 | }
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| 330 | printLine(line, coTime);
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| 331 | }
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| 332 | }
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| 333 |
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| 334 | retCode = success;
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| 335 | memset(&_co, 0, sizeof(_co));
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| 336 | memset(&_bias, 0, sizeof(_bias));
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| 337 | }
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| 338 | }
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| 339 | }
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| 340 |
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| 341 | if (retCode != success) {
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| 342 | _GPSweeks = -1.0;
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| 343 | }
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| 344 | return retCode;
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| 345 | }
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| 346 |
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| 347 | //
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| 348 | ////////////////////////////////////////////////////////////////////////////
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| 349 | void RTCM3coDecoder::printLine(const QString& line, long coTime) {
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| 350 | if (_out) {
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| 351 | *_out << line.toAscii().data() << endl;
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| 352 | _out->flush();
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| 353 | }
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| 354 |
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| 355 | emit newCorrLine(line, _staID, coTime);
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| 356 | }
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