| 1 |
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| 2 | #include <iostream>
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| 3 | #include <iomanip>
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| 4 | #include <string.h>
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| 5 |
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| 6 | #include "bncrtrover.h"
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| 7 | #include "bnccore.h"
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| 8 | #include "bncsettings.h"
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| 9 | #include "bnctime.h"
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| 10 |
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| 11 | #include "rtrover_interface.h"
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| 12 |
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| 13 | using namespace std;
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| 14 |
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| 15 | // Constructor
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| 16 | ////////////////////////////////////////////////////////////////////////////
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| 17 | t_bncRtrover::t_bncRtrover() : QThread(0) {
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| 18 | }
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| 19 |
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| 20 | // Destructor
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| 21 | ////////////////////////////////////////////////////////////////////////////
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| 22 | t_bncRtrover::~t_bncRtrover() {
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| 23 | rtrover_destroy();
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| 24 | }
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| 25 |
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| 26 | // Run (virtual)
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| 27 | ////////////////////////////////////////////////////////////////////////////
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| 28 | void t_bncRtrover::run() {
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| 29 | bncSettings settings;
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| 30 |
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| 31 | // User Options
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| 32 | // ------------
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| 33 | _mode = settings.value("rtroverMode").toByteArray();
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| 34 | _roverMount = settings.value("rtroverRoverMount").toByteArray();
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| 35 | _baseMount = settings.value("rtroverBaseMount").toByteArray();
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| 36 | _corrMount = settings.value("rtroverCorrMount").toByteArray();
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| 37 | _outputFile.setFileName(settings.value("rtroverOutput").toString());
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| 38 | _outputFile.open(QIODevice::WriteOnly | QIODevice::Text);
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| 39 |
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| 40 | // Define Input Options
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| 41 | // --------------------
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| 42 | rtrover_opt opt;
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| 43 | rtrover_initOptions(&opt);
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| 44 |
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| 45 | if (_mode == "PPP_DF") {
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| 46 | opt._mode = mode_PPP_DF;
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| 47 | }
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| 48 | else if (_mode == "SPP_DF") {
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| 49 | opt._mode = mode_SPP_DF;
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| 50 | }
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| 51 | else if (_mode == "PPP_SF") {
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| 52 | opt._mode = mode_PPP_SF;
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| 53 | }
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| 54 | else if (_mode == "SPP_SF") {
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| 55 | opt._mode = mode_SPP_SF;
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| 56 | }
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| 57 | else if (_mode == "PPP_AR") {
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| 58 | opt._mode = mode_PPP_AR;
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| 59 | }
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| 60 | else if (_mode == "RTK") {
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| 61 | opt._mode = mode_RTK;
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| 62 | }
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| 63 | else if (_mode == "PPP_FTTF") {
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| 64 | opt._mode = mode_PPP_FTTF;
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| 65 | }
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| 66 |
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| 67 | QByteArray antNameRover = settings.value("rtroverRoverAntenna").toByteArray();
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| 68 | QByteArray antNameBase = settings.value("rtroverBaseAntenna").toByteArray();
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| 69 | QByteArray antexFileName = settings.value("rtroverAntex").toByteArray();
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| 70 |
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| 71 | if (!_roverMount.isEmpty()) opt._roverName = _roverMount.data();
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| 72 | if (!_baseMount.isEmpty()) opt._baseName = _baseMount.data();
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| 73 | if (!antNameRover.isEmpty()) opt._antNameRover = antNameRover.data();
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| 74 | if (!antNameBase.isEmpty()) opt._antNameBase = antNameBase.data();
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| 75 | if (!antexFileName.isEmpty()) opt._antexFileName = antexFileName.data();
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| 76 |
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| 77 | opt._xyzAprRover[0] = settings.value("rtroverRoverRefCrdX").toDouble();
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| 78 | opt._xyzAprRover[1] = settings.value("rtroverRoverRefCrdY").toDouble();
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| 79 | opt._xyzAprRover[2] = settings.value("rtroverRoverRefCrdZ").toDouble();
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| 80 | opt._xyzAprBase[0] = settings.value("rtroverBaseRefCrdX").toDouble();
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| 81 | opt._xyzAprBase[1] = settings.value("rtroverBaseRefCrdY").toDouble();
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| 82 | opt._xyzAprBase[2] = settings.value("rtroverBaseRefCrdZ").toDouble();
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| 83 | opt._neuEccRover[0] = settings.value("rtroverRoverDN").toDouble();
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| 84 | opt._neuEccRover[1] = settings.value("rtroverRoverDE").toDouble();
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| 85 | opt._neuEccRover[2] = settings.value("rtroverRoverDU").toDouble();
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| 86 | opt._neuEccBase[0] = settings.value("rtroverBaseDN").toDouble();
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| 87 | opt._neuEccBase[1] = settings.value("rtroverBaseDE").toDouble();
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| 88 | opt._neuEccBase[2] = settings.value("rtroverBaseDU").toDouble();
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| 89 | opt._logLevel = 2;
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| 90 |
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| 91 | rtrover_setOptions(&opt);
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| 92 |
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| 93 | // Connect to BNC Signals
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| 94 | // ----------------------
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| 95 | connect(BNC_CORE, SIGNAL(newCorrections(QList<QString>)),
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| 96 | this, SLOT(slotNewCorrections(QList<QString>)));
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| 97 |
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| 98 | connect(BNC_CORE, SIGNAL(newEphGPS(gpsephemeris)),
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| 99 | this, SLOT(slotNewEphGPS(gpsephemeris)));
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| 100 |
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| 101 | connect(BNC_CORE, SIGNAL(newEphGlonass(glonassephemeris)),
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| 102 | this, SLOT(slotNewEphGlonass(glonassephemeris)));
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| 103 |
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| 104 | connect(BNC_CORE, SIGNAL(newEphGalileo(galileoephemeris)),
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| 105 | this, SLOT(slotNewEphGalileo(galileoephemeris)));
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| 106 |
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| 107 | // Start processing loop
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| 108 | // ---------------------
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| 109 | QThread::exec();
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| 110 | }
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| 111 |
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| 112 | //
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| 113 | ////////////////////////////////////////////////////////////////////////////
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| 114 | void t_bncRtrover::slotNewEphGPS(gpsephemeris gpseph) {
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| 115 | QMutexLocker locker(&_mutex);
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| 116 |
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| 117 | bncTime toc(gpseph.GPSweek, gpseph.TOC);
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| 118 | bncTime toe(gpseph.GPSweek, gpseph.TOE);
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| 119 |
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| 120 | rtrover_ephGPS eph;
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| 121 | eph._satellite._system = 'G';
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| 122 | eph._satellite._number = gpseph.satellite;
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| 123 | eph._TOC._mjd = toc.mjd();
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| 124 | eph._TOC._sec = toc.daysec();
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| 125 | eph._TOE._mjd = toe.mjd();
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| 126 | eph._TOE._sec = toe.daysec();
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| 127 | eph._IODE = gpseph.IODE;
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| 128 | eph._IODC = gpseph.IODC;
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| 129 | eph._clock_bias = gpseph.clock_bias;
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| 130 | eph._clock_drift = gpseph.clock_drift;
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| 131 | eph._clock_driftrate = gpseph.clock_driftrate;
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| 132 | eph._Crs = gpseph.Crs;
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| 133 | eph._Delta_n = gpseph.Delta_n;
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| 134 | eph._M0 = gpseph.M0;
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| 135 | eph._Cuc = gpseph.Cuc;
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| 136 | eph._e = gpseph.e;
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| 137 | eph._Cus = gpseph.Cus;
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| 138 | eph._sqrt_A = gpseph.sqrt_A;
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| 139 | eph._Cic = gpseph.Cic;
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| 140 | eph._OMEGA0 = gpseph.OMEGA0;
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| 141 | eph._Cis = gpseph.Cis;
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| 142 | eph._i0 = gpseph.i0;
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| 143 | eph._Crc = gpseph.Crc;
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| 144 | eph._omega = gpseph.omega;
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| 145 | eph._OMEGADOT = gpseph.OMEGADOT;
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| 146 | eph._IDOT = gpseph.IDOT;
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| 147 | eph._TGD = gpseph.TGD;
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| 148 | eph._health = gpseph.SVhealth;
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| 149 |
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| 150 | rtrover_putGPSEphemeris(&eph);
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| 151 | }
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| 152 |
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| 153 | //
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| 154 | ////////////////////////////////////////////////////////////////////////////
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| 155 | void t_bncRtrover::slotNewEphGlonass(glonassephemeris gloeph) {
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| 156 | QMutexLocker locker(&_mutex);
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| 157 |
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| 158 | int wwUTC = gloeph.GPSWeek;
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| 159 | int towUTC = gloeph.GPSTOW;
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| 160 | updatetime(&wwUTC, &towUTC, gloeph.tb*1000, 1); // Moscow -> UTC
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| 161 | bncTime tUTC(wwUTC,towUTC);
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| 162 |
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| 163 | int wwGPS = gloeph.GPSWeek;
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| 164 | int towGPS = gloeph.GPSTOW;
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| 165 | updatetime(&wwGPS, &towGPS, gloeph.tb*1000, 0); // Moscow -> GPS
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| 166 | bncTime tGPS(wwGPS,towGPS);
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| 167 |
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| 168 | rtrover_ephGlo eph;
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| 169 | eph._satellite._system = 'R';
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| 170 | eph._satellite._number = gloeph.almanac_number;
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| 171 | eph._timeUTC._mjd = tUTC.mjd();
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| 172 | eph._timeUTC._sec = tUTC.daysec();
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| 173 | eph._gps_utc = int(tGPS-tUTC);
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| 174 | eph._E = gloeph.E;
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| 175 | eph._tau = gloeph.tau;
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| 176 | eph._gamma = gloeph.gamma;
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| 177 | eph._x_pos = gloeph.x_pos;
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| 178 | eph._x_velocity = gloeph.x_velocity;
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| 179 | eph._x_acceleration = gloeph.x_acceleration;
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| 180 | eph._y_pos = gloeph.y_pos;
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| 181 | eph._y_velocity = gloeph.y_velocity;
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| 182 | eph._y_acceleration = gloeph.y_acceleration;
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| 183 | eph._z_pos = gloeph.z_pos;
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| 184 | eph._z_velocity = gloeph.z_velocity;
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| 185 | eph._z_acceleration = gloeph.z_acceleration;
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| 186 | eph._health = 0; // TODO ?
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| 187 | eph._frequency_number = gloeph.frequency_number;
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| 188 |
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| 189 | rtrover_putGloEphemeris(&eph);
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| 190 | }
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| 191 |
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| 192 | //
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| 193 | ////////////////////////////////////////////////////////////////////////////
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| 194 | void t_bncRtrover::slotNewEphGalileo(galileoephemeris /* galeph */) {
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| 195 | // not yet implemented
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| 196 | }
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| 197 |
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| 198 | //
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| 199 | ////////////////////////////////////////////////////////////////////////////
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| 200 | void t_bncRtrover::slotNewCorrections(QList<QString> corrList) {
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| 201 | QMutexLocker locker(&_mutex);
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| 202 |
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| 203 | if (corrList.size() == 0) {
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| 204 | return;
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| 205 | }
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| 206 |
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| 207 | int numOrbCorr = 0;
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| 208 | int numClkCorr = 0;
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| 209 | int numBiases = 0;
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| 210 |
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| 211 | rtrover_orbCorr orbCorr[corrList.size()];
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| 212 | rtrover_clkCorr clkCorr[corrList.size()];
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| 213 | rtrover_satBiases biases[corrList.size()];
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| 214 |
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| 215 | QListIterator<QString> it(corrList);
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| 216 | while (it.hasNext()) {
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| 217 | QString line = it.next();
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| 218 |
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| 219 | // Check the Mountpoint
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| 220 | // --------------------
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| 221 | QStringList hlp = line.split(" ");
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| 222 | if (hlp.size() > 0) {
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| 223 | QString mountpoint = hlp[hlp.size()-1];
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| 224 | if (mountpoint != _corrMount) {
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| 225 | continue;
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| 226 | }
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| 227 | }
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| 228 |
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| 229 | // Orbit and clock corrections
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| 230 | // ---------------------------
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| 231 | t_corr corr;
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| 232 | if (corr.readLine(line) == success) {
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| 233 |
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| 234 | if (corr.messageType == COTYPE_GPSCOMBINED ||
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| 235 | corr.messageType == COTYPE_GLONASSCOMBINED ||
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| 236 | corr.messageType == COTYPE_GPSORBIT ||
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| 237 | corr.messageType == COTYPE_GLONASSORBIT ) {
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| 238 |
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| 239 | _IODs[corr.prn] = corr.iod; // remember iod;
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| 240 |
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| 241 | ++numOrbCorr;
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| 242 | rtrover_orbCorr& orbC = orbCorr[numOrbCorr-1];
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| 243 | orbC._satellite._system = corr.prn.toAscii()[0];
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| 244 | orbC._satellite._number = corr.prn.mid(1).toInt();
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| 245 | orbC._iod = corr.iod;
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| 246 | orbC._time._mjd = corr.tRao.mjd();
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| 247 | orbC._time._sec = corr.tRao.daysec();
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| 248 | for (int ii = 0; ii < 3; ii++) {
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| 249 | orbC._rao[ii] = corr.rao[ii];
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| 250 | orbC._dotRao[ii] = corr.dotRao[ii];
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| 251 | orbC._dotDotRao[ii] = corr.dotDotRao[ii];
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| 252 | }
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| 253 | }
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| 254 |
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| 255 | if (corr.messageType == COTYPE_GPSCOMBINED ||
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| 256 | corr.messageType == COTYPE_GLONASSCOMBINED ||
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| 257 | corr.messageType == COTYPE_GPSCLOCK ||
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| 258 | corr.messageType == COTYPE_GLONASSCLOCK ) {
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| 259 | ++numClkCorr;
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| 260 | rtrover_clkCorr& clkC = clkCorr[numClkCorr-1];
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| 261 | clkC._satellite._system = corr.prn.toAscii()[0];
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| 262 | clkC._satellite._number = corr.prn.mid(1).toInt();
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| 263 | if (_IODs.contains(corr.prn)) {
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| 264 | clkC._iod = _IODs[corr.prn];
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| 265 | }
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| 266 | else {
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| 267 | clkC._iod = 0;
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| 268 | }
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| 269 | clkC._time._mjd = corr.tClk.mjd();
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| 270 | clkC._time._sec = corr.tClk.daysec();
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| 271 | clkC._dClk = corr.dClk;
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| 272 | clkC._dotDClk = corr.dotDClk;
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| 273 | clkC._dotDotDClk = corr.dotDotDClk;
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| 274 | }
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| 275 | }
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| 276 |
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| 277 | // Code Biases
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| 278 | // -----------
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| 279 | t_bias bias;
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| 280 | if (bias.readLine(line) == success) {
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| 281 | ++numBiases;
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| 282 | rtrover_satBiases& satBiases = biases[numBiases-1];
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| 283 | satBiases._satellite._system = bias._prn.toAscii()[0];
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| 284 | satBiases._satellite._number = bias._prn.mid(1).toInt();
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| 285 | satBiases._time._mjd = bias._time.mjd();
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| 286 | satBiases._time._sec = bias._time.daysec();
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| 287 | satBiases._numBiases = bias._value.size();
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| 288 | satBiases._biases = new rtrover_bias[satBiases._numBiases];
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| 289 | int iBias = -1;
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| 290 | QMapIterator<QByteArray, double> it(bias._value);
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| 291 | while (it.hasNext()) {
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| 292 | it.next();
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| 293 | ++iBias;
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| 294 | rtrover_bias& singleBias = satBiases._biases[iBias];
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| 295 | singleBias._rnxType3ch[0] = 'C';
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| 296 | singleBias._rnxType3ch[1] = it.key()[0];
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| 297 | singleBias._rnxType3ch[2] = it.key()[1];
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| 298 | singleBias._value = it.value();
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| 299 | }
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| 300 | }
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| 301 | }
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| 302 |
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| 303 | // Pass Corrections and Biases to client library
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| 304 | // ---------------------------------------------
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| 305 | if (numOrbCorr > 0) {
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| 306 | rtrover_putOrbCorrections(numOrbCorr, orbCorr);
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| 307 | }
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| 308 | if (numClkCorr > 0) {
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| 309 | rtrover_putClkCorrections(numClkCorr, clkCorr);
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| 310 | }
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| 311 | if (numBiases > 0) {
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| 312 | rtrover_putBiases(numBiases, biases);
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| 313 | }
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| 314 |
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| 315 | // Clean the memory
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| 316 | // ----------------
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| 317 | for (int ii = 0; ii < numBiases; ii++) {
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| 318 | delete [] biases[ii]._biases;
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| 319 | }
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| 320 | }
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| 321 |
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| 322 | // Auxiliary function - copy observation data
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| 323 | ////////////////////////////////////////////////////////////////////////////
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| 324 | void copyObs(const t_obs& obsBnc, rtrover_satObs& satObs) {
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| 325 |
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| 326 | bncTime obsTime(obsBnc.GPSWeek, obsBnc.GPSWeeks);
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| 327 | satObs._satellite._system = obsBnc.satSys;
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| 328 | satObs._satellite._number = obsBnc.satNum;
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| 329 | satObs._time._mjd = obsTime.mjd();
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| 330 | satObs._time._sec = obsTime.daysec();
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| 331 | satObs._slotNumber = obsBnc.slotNum;
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| 332 |
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| 333 | QMap<QByteArray, rtrover_obs> allObs;
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| 334 | for (int iEntry = 0; iEntry < GNSSENTRY_NUMBER; ++iEntry) {
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| 335 | if (obsBnc._measdata[iEntry] != 0.0) {
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| 336 | QByteArray rnxStr = obsBnc.rnxStr(iEntry).toAscii();
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| 337 | if (rnxStr.length() == 3) {
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| 338 | QByteArray codeType = rnxStr.mid(1);
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| 339 |
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| 340 | bool existed = allObs.contains(codeType);
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| 341 | rtrover_obs& currObs = allObs[codeType];
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| 342 | if (!existed) {
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| 343 | rtrover_initObs(&currObs);
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| 344 | currObs._rnxType2ch[0] = codeType[0];
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| 345 | currObs._rnxType2ch[1] = codeType[1];
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| 346 | }
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| 347 |
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| 348 | if (rnxStr[0] == 'C') {
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| 349 | currObs._code = obsBnc._measdata[iEntry];
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| 350 | currObs._codeValid = true;
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| 351 | }
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| 352 | else if (rnxStr[0] == 'L') {
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| 353 | currObs._phase = obsBnc._measdata[iEntry];
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| 354 | currObs._phaseValid = true;
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| 355 | if (codeType[0] == '1') {
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| 356 | currObs._slip = obsBnc.slipL1;
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| 357 | currObs._slipCounter = obsBnc.slip_cnt_L1;
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| 358 | }
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| 359 | else if (codeType[0] == '2') {
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| 360 | currObs._slip = obsBnc.slipL2;
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| 361 | currObs._slipCounter = obsBnc.slip_cnt_L2;
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| 362 | }
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| 363 | else if (codeType[0] == '5') {
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| 364 | currObs._slip = obsBnc.slipL5;
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| 365 | currObs._slipCounter = obsBnc.slip_cnt_L5;
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| 366 | }
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| 367 | }
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| 368 | else if (rnxStr[0] == 'D') {
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| 369 | currObs._doppler = obsBnc._measdata[iEntry];
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| 370 | currObs._dopplerValid = true;
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| 371 | }
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| 372 | else if (rnxStr[0] == 'S') {
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| 373 | currObs._snr = obsBnc._measdata[iEntry];
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| 374 | currObs._snrValid = true;
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| 375 | }
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| 376 | }
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| 377 | }
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| 378 | }
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| 379 | satObs._numObs = allObs.size();
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| 380 | satObs._obs = new rtrover_obs[satObs._numObs];
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| 381 | int iObs = -1;
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| 382 | QMapIterator<QByteArray, rtrover_obs> it(allObs);
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| 383 | while (it.hasNext()) {
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| 384 | it.next();
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| 385 | ++iObs;
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| 386 | satObs._obs[iObs] = it.value();
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| 387 | }
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| 388 | }
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| 389 |
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| 390 | //
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| 391 | ////////////////////////////////////////////////////////////////////////////
|
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| 392 | void t_bncRtrover::slotNewObs(QByteArray staID, bool /* firstObs */, t_obs obsIn) {
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| 393 | QMutexLocker locker(&_mutex);
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| 394 |
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| 395 | if (staID != _roverMount && staID != _baseMount) {
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| 396 | return;
|
|---|
| 397 | }
|
|---|
| 398 |
|
|---|
| 399 | bncTime obsTime(obsIn.GPSWeek, obsIn.GPSWeeks);
|
|---|
| 400 |
|
|---|
| 401 | // Find corresponding epoch or create a new one
|
|---|
| 402 | // --------------------------------------------
|
|---|
| 403 | t_epoData* epoData = 0;
|
|---|
| 404 | for (unsigned ii = 0; ii < _epochs.size(); ii++) {
|
|---|
| 405 | if (_epochs[ii]->_time == obsTime) {
|
|---|
| 406 | epoData = _epochs[ii];
|
|---|
| 407 | break;
|
|---|
| 408 | }
|
|---|
| 409 | }
|
|---|
| 410 | if (epoData == 0) {
|
|---|
| 411 | if (_epochs.size() == 0 || _epochs.back()->_time < obsTime) {
|
|---|
| 412 | epoData = new t_epoData();
|
|---|
| 413 | epoData->_time = obsTime;
|
|---|
| 414 | _epochs.push_back(epoData);
|
|---|
| 415 | }
|
|---|
| 416 | else {
|
|---|
| 417 | return;
|
|---|
| 418 | }
|
|---|
| 419 | }
|
|---|
| 420 |
|
|---|
| 421 | // Store observation into epoch class
|
|---|
| 422 | // ----------------------------------
|
|---|
| 423 | if (staID == _roverMount) {
|
|---|
| 424 | epoData->_obsRover.push_back(obsIn);
|
|---|
| 425 | }
|
|---|
| 426 | else if (staID == _baseMount) {
|
|---|
| 427 | epoData->_obsBase.push_back(obsIn);
|
|---|
| 428 | }
|
|---|
| 429 |
|
|---|
| 430 | // Wait for observations
|
|---|
| 431 | // ---------------------
|
|---|
| 432 | const double WAITTIME = 5.0;
|
|---|
| 433 | double dt = 0.0;
|
|---|
| 434 | if (_epochs.size() > 1) {
|
|---|
| 435 | dt = _epochs.back()->_time - _epochs.front()->_time;
|
|---|
| 436 | }
|
|---|
| 437 | if (dt < WAITTIME) {
|
|---|
| 438 | return;
|
|---|
| 439 | }
|
|---|
| 440 |
|
|---|
| 441 | // Copy observations into rtrover_satObs structures
|
|---|
| 442 | // ------------------------------------------------
|
|---|
| 443 | t_epoData* frontEpoData = _epochs.front();
|
|---|
| 444 | _epochs.erase(_epochs.begin());
|
|---|
| 445 |
|
|---|
| 446 | int numSatRover = frontEpoData->_obsRover.size();
|
|---|
| 447 | rtrover_satObs satObsRover[numSatRover];
|
|---|
| 448 | for (int ii = 0; ii < numSatRover; ii++) {
|
|---|
| 449 | const t_obs& obsBnc = frontEpoData->_obsRover[ii];
|
|---|
| 450 | rtrover_satObs& satObs = satObsRover[ii];
|
|---|
| 451 | copyObs(obsBnc, satObs);
|
|---|
| 452 | }
|
|---|
| 453 |
|
|---|
| 454 | int numSatBase = frontEpoData->_obsBase.size();
|
|---|
| 455 | rtrover_satObs satObsBase[numSatBase];
|
|---|
| 456 | for (int ii = 0; ii < numSatBase; ii++) {
|
|---|
| 457 | const t_obs& obsBnc = frontEpoData->_obsBase[ii];
|
|---|
| 458 | rtrover_satObs& satObs = satObsBase[ii];
|
|---|
| 459 | copyObs(obsBnc, satObs);
|
|---|
| 460 | }
|
|---|
| 461 |
|
|---|
| 462 | delete frontEpoData;
|
|---|
| 463 |
|
|---|
| 464 | // Process single epoch
|
|---|
| 465 | // --------------------
|
|---|
| 466 | rtrover_output output;
|
|---|
| 467 | rtrover_processEpoch(numSatRover, satObsRover, numSatBase, satObsBase, &output);
|
|---|
| 468 |
|
|---|
| 469 | // Write output
|
|---|
| 470 | // ---------------------
|
|---|
| 471 | _outputFile.write(output._log);
|
|---|
| 472 | _outputFile.flush();
|
|---|
| 473 |
|
|---|
| 474 | // Free memory
|
|---|
| 475 | // -----------
|
|---|
| 476 | rtrover_freeOutput(&output);
|
|---|
| 477 | for (int ii = 0; ii < numSatRover; ii++) {
|
|---|
| 478 | rtrover_satObs& satObs = satObsRover[ii];
|
|---|
| 479 | delete [] satObs._obs;
|
|---|
| 480 | }
|
|---|
| 481 | for (int ii = 0; ii < numSatBase; ii++) {
|
|---|
| 482 | rtrover_satObs& satObs = satObsBase[ii];
|
|---|
| 483 | delete [] satObs._obs;
|
|---|
| 484 | }
|
|---|
| 485 | }
|
|---|