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: bncRtnetDecoder
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30 | *
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31 | * Purpose: Implementation of RTNet (SP3-like) output 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: 28-Mar-2011
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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 <iostream>
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42 | #include "bncrtnetdecoder.h"
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43 | #include "bncutils.h"
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44 | #include "bncsettings.h"
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45 |
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46 | using namespace std;
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47 |
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48 | // Constructor
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49 | ////////////////////////////////////////////////////////////////////////
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50 | bncRtnetDecoder::bncRtnetDecoder() {
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51 | bncSettings settings;
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52 | _year = 0;
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53 | }
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54 |
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55 | // Destructor
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56 | ////////////////////////////////////////////////////////////////////////
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57 | bncRtnetDecoder::~bncRtnetDecoder() {
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58 | }
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59 |
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60 | //
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61 | ////////////////////////////////////////////////////////////////////////
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62 | void bncRtnetDecoder::readEpochTime(const QString& line) {
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63 | QTextStream in(line.toAscii());
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64 | QString hlp;
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65 | in >> hlp >> _year >> _month >> _day >> _hour >> _min >> _sec;
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66 | GPSweekFromYMDhms(_year, _month, _day, _hour, _min, _sec, _GPSweek, _GPSweeks);
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67 | }
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68 |
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69 | // Decode Method
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70 | ////////////////////////////////////////////////////////////////////////
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71 | t_irc bncRtnetDecoder::Decode(char* buffer, int bufLen, vector<string>& errmsg) {
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72 |
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73 | errmsg.clear();
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74 | _buffer.append(QByteArray(buffer, bufLen));
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75 |
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76 | // Prepare list of lines with satellite positions in SP3-like format
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77 | // -----------------------------------------------------------------
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78 | QStringList lines;
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79 | int iLast = _buffer.lastIndexOf('\n');
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80 | if (iLast != -1) {
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81 | QStringList hlpLines = _buffer.split('\n', QString::SkipEmptyParts);
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82 | _buffer = _buffer.mid(iLast+1);
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83 | for (int ii = 0; ii < hlpLines.size(); ii++) {
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84 | if (hlpLines[ii].indexOf('*') != -1) {
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85 | readEpochTime(hlpLines[ii]);
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86 | }
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87 | else if (_year != 0) {
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88 | lines << hlpLines[ii];
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89 | }
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90 | }
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91 | }
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92 |
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93 | // Satellite positions to be processed
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94 | // -----------------------------------
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95 | if (lines.size() > 0) {
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96 |
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97 | QStringList prns;
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98 |
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99 | for (int ic = 0; ic < _caster.size(); ic++) {
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100 | _caster.at(ic)->open();
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101 |
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102 | struct ClockOrbit co;
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103 | memset(&co, 0, sizeof(co));
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104 | co.GPSEpochTime = (int)_GPSweeks;
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105 | co.GLONASSEpochTime = (int)fmod(_GPSweeks, 86400.0)
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106 | + 3 * 3600 - gnumleap(_year, _month, _day);
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107 | co.ClockDataSupplied = 1;
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108 | co.OrbitDataSupplied = 1;
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109 | co.SatRefDatum = DATUM_ITRF;
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110 |
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111 | struct Bias bias;
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112 | memset(&bias, 0, sizeof(bias));
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113 | bias.GPSEpochTime = (int)_GPSweeks;
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114 | bias.GLONASSEpochTime = (int)fmod(_GPSweeks, 86400.0)
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115 | + 3 * 3600 - gnumleap(_year, _month, _day);
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116 |
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117 | for (int ii = 0; ii < lines.size(); ii++) {
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118 |
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119 | QString prn;
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120 | ColumnVector xx(14); xx = 0.0;
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121 | t_ephPair* pair = 0;
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122 |
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123 | if (ic == 0) {
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124 | QTextStream in(lines[ii].toAscii());
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125 | in >> prn;
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126 | prns << prn;
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127 | if ( _ephList.contains(prn) ) {
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128 | in >> xx(1) >> xx(2) >> xx(3) >> xx(4) >> xx(5)
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129 | >> xx(6) >> xx(7) >> xx(8) >> xx(9) >> xx(10)
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130 | >> xx(11) >> xx(12) >> xx(13) >> xx(14);
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131 | xx(1) *= 1e3; // x-crd
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132 | xx(2) *= 1e3; // y-crd
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133 | xx(3) *= 1e3; // z-crd
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134 | xx(4) *= 1e-6; // clk
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135 | xx(5) *= 1e-6; // rel. corr.
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136 | // xx(6), xx(7), xx(8) ... PhaseCent - CoM
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137 | // xx(9) ... P1-C1 DCB in meters
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138 | // xx(10) ... P1-P2 DCB in meters
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139 | // xx(11) ... dT
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140 | xx(12) *= 1e3; // x-crd at time + dT
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141 | xx(13) *= 1e3; // y-crd at time + dT
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142 | xx(14) *= 1e3; // z-crd at time + dT
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143 |
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144 | pair = _ephList[prn];
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145 | pair->xx = xx;
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146 | }
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147 | }
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148 | else {
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149 | prn = prns[ii];
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150 | if ( _ephList.contains(prn) ) {
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151 | pair = _ephList[prn];
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152 | xx = pair->xx;
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153 | }
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154 | }
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155 |
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156 | // Use old ephemeris if the new one is too recent
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157 | // ----------------------------------------------
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158 | t_eph* ep = 0;
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159 | if (pair) {
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160 | ep = pair->eph;
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161 | if (pair->oldEph && ep &&
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162 | ep->receptDateTime().secsTo(QDateTime::currentDateTime()) < 60) {
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163 | ep = pair->oldEph;
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164 | }
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165 | }
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166 |
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167 | if (ep != 0) {
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168 | struct ClockOrbit::SatData* sd = 0;
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169 | if (prn[0] == 'G') {
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170 | sd = co.Sat + co.NumberOfGPSSat;
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171 | ++co.NumberOfGPSSat;
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172 | }
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173 | else if (prn[0] == 'R') {
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174 | sd = co.Sat + CLOCKORBIT_NUMGPS + co.NumberOfGLONASSSat;
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175 | ++co.NumberOfGLONASSSat;
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176 | }
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177 | if (sd) {
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178 | QString outLine;
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179 | processSatellite(ic, _caster.at(ic)->crdTrafo(),
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180 | _caster.at(ic)->CoM(), ep,
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181 | _GPSweek, _GPSweeks, prn, xx, sd, outLine);
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182 | _caster.at(ic)->printAscii(outLine);
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183 | }
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184 |
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185 | struct Bias::BiasSat* biasSat = 0;
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186 | if (prn[0] == 'G') {
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187 | biasSat = bias.Sat + bias.NumberOfGPSSat;
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188 | ++bias.NumberOfGPSSat;
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189 | }
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190 | else if (prn[0] == 'R') {
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191 | biasSat = bias.Sat + CLOCKORBIT_NUMGPS + bias.NumberOfGLONASSSat;
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192 | ++bias.NumberOfGLONASSSat;
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193 | }
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194 |
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195 | // Coefficient of Ionosphere-Free LC
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196 | // ---------------------------------
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197 | const static double a_L1_GPS = 2.54572778;
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198 | const static double a_L2_GPS = -1.54572778;
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199 | const static double a_L1_Glo = 2.53125000;
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200 | const static double a_L2_Glo = -1.53125000;
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201 |
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202 | if (biasSat) {
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203 | biasSat->ID = prn.mid(1).toInt();
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204 | biasSat->NumberOfCodeBiases = 3;
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205 | if (prn[0] == 'G') {
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206 | biasSat->Biases[0].Type = CODETYPEGPS_L1_Z;
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207 | biasSat->Biases[0].Bias = - a_L2_GPS * xx(10);
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208 | biasSat->Biases[1].Type = CODETYPEGPS_L1_CA;
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209 | biasSat->Biases[1].Bias = - a_L2_GPS * xx(10) + xx(9);
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210 | biasSat->Biases[2].Type = CODETYPEGPS_L2_Z;
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211 | biasSat->Biases[2].Bias = a_L1_GPS * xx(10);
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212 | }
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213 | else if (prn[0] == 'R') {
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214 | biasSat->Biases[0].Type = CODETYPEGLONASS_L1_P;
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215 | biasSat->Biases[0].Bias = - a_L2_Glo * xx(10);
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216 | biasSat->Biases[1].Type = CODETYPEGLONASS_L1_CA;
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217 | biasSat->Biases[1].Bias = - a_L2_Glo * xx(10) + xx(9);
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218 | biasSat->Biases[2].Type = CODETYPEGLONASS_L2_P;
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219 | biasSat->Biases[2].Bias = a_L1_Glo * xx(10);
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220 | }
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221 | }
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222 | }
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223 | }
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224 |
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225 | if ( _caster.at(ic)->usedSocket() &&
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226 | (co.NumberOfGPSSat > 0 || co.NumberOfGLONASSSat > 0) ) {
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227 | char obuffer[CLOCKORBIT_BUFFERSIZE];
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228 |
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229 | int len = MakeClockOrbit(&co, COTYPE_AUTO, 0, obuffer, sizeof(obuffer));
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230 | if (len > 0) {
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231 | if (_caster.at(ic)->ic() == 1) { emit(newOutBytes1(len));}
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232 | if (_caster.at(ic)->ic() == 2) { emit(newOutBytes2(len));}
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233 | if (_caster.at(ic)->ic() == 3) { emit(newOutBytes3(len));}
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234 | if (_caster.at(ic)->ic() == 4) { emit(newOutBytes4(len));}
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235 | if (_caster.at(ic)->ic() == 5) { emit(newOutBytes5(len));}
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236 | if (_caster.at(ic)->ic() == 6) { emit(newOutBytes6(len));}
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237 | if (_caster.at(ic)->ic() == 7) { emit(newOutBytes7(len));}
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238 | if (_caster.at(ic)->ic() == 8) { emit(newOutBytes8(len));}
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239 | if (_caster.at(ic)->ic() == 9) { emit(newOutBytes9(len));}
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240 | if (_caster.at(ic)->ic() == 10) { emit(newOutBytes10(len));}
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241 | _caster.at(ic)->write(obuffer, len);
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242 | }
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243 | }
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244 |
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245 | if ( _caster.at(ic)->usedSocket() &&
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246 | (bias.NumberOfGPSSat > 0 || bias.NumberOfGLONASSSat > 0) ) {
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247 | char obuffer[CLOCKORBIT_BUFFERSIZE];
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248 | int len = MakeBias(&bias, BTYPE_AUTO, 0, obuffer, sizeof(obuffer));
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249 | if (len > 0) {
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250 | _caster.at(ic)->write(obuffer, len);
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251 | }
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252 | }
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253 | }
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254 | }
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255 |
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256 | return success;
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257 | }
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258 |
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259 | //
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260 | ////////////////////////////////////////////////////////////////////////////
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261 | void bncRtnetDecoder::processSatellite(int iCaster, const QString trafo,
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262 | bool CoM, t_eph* ep, int GPSweek,
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263 | double GPSweeks, const QString& prn,
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264 | const ColumnVector& xx,
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265 | struct ClockOrbit::SatData* sd,
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266 | QString& outLine) {
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267 |
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268 | const double secPerWeek = 7.0 * 86400.0;
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269 |
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270 | ColumnVector rsw(3);
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271 | ColumnVector rsw2(3);
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272 | double dClk;
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273 |
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274 | for (int ii = 1; ii <= 2; ++ii) {
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275 |
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276 | int GPSweek12 = GPSweek;
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277 | double GPSweeks12 = GPSweeks;
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278 | if (ii == 2) {
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279 | GPSweeks12 += xx(11);
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280 | if (GPSweeks12 > secPerWeek) {
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281 | GPSweek12 += 1;
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282 | GPSweeks12 -= secPerWeek;
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283 | }
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284 | }
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285 |
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286 | ColumnVector xB(4);
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287 | ColumnVector vv(3);
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288 |
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289 | ep->position(GPSweek12, GPSweeks12, xB, vv);
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290 |
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291 | ColumnVector xyz;
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292 | if (ii == 1) {
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293 | xyz = xx.Rows(1,3);
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294 | }
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295 | else {
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296 | xyz = xx.Rows(12,14);
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297 | }
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298 |
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299 | // Correction Center of Mass -> Antenna Phase Center
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300 | // -------------------------------------------------
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301 | if (! CoM) {
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302 | xyz(1) += xx(6);
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303 | xyz(2) += xx(7);
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304 | xyz(3) += xx(8);
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305 | }
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306 |
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307 | if (trafo != "IGS05") {
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308 | crdTrafo(GPSweek12, xyz, trafo);
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309 | }
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310 |
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311 | ColumnVector dx = xB.Rows(1,3) - xyz ;
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312 |
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313 | if (ii == 1) {
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314 | XYZ_to_RSW(xB.Rows(1,3), vv, dx, rsw);
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315 | dClk = (xx(4) + xx(5) - xB(4)) * 299792458.0;
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316 | }
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317 | else {
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318 | XYZ_to_RSW(xB.Rows(1,3), vv, dx, rsw2);
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319 | }
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320 | }
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321 |
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322 | if (sd) {
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323 | sd->ID = prn.mid(1).toInt();
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324 | sd->IOD = ep->IOD();
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325 | sd->Clock.DeltaA0 = dClk;
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326 | sd->Orbit.DeltaRadial = rsw(1);
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327 | sd->Orbit.DeltaAlongTrack = rsw(2);
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328 | sd->Orbit.DeltaCrossTrack = rsw(3);
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329 | sd->Orbit.DotDeltaRadial = (rsw2(1) - rsw(1)) / xx(11);
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330 | sd->Orbit.DotDeltaAlongTrack = (rsw2(2) - rsw(2)) / xx(11);
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331 | sd->Orbit.DotDeltaCrossTrack = (rsw2(3) - rsw(3)) / xx(11);
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332 | }
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333 |
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334 | outLine.sprintf("%d %.1f %s %3d %10.3f %8.3f %8.3f %8.3f\n",
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335 | GPSweek, GPSweeks, ep->prn().toAscii().data(),
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336 | ep->IOD(), dClk, rsw(1), rsw(2), rsw(3));
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337 |
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338 | if (iCaster == 0) {
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339 | if (_rnx) {
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340 | _rnx->write(GPSweek, GPSweeks, prn, xx);
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341 | }
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342 | if (_sp3) {
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343 | _sp3->write(GPSweek, GPSweeks, prn, xx, _append);
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344 | }
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345 | }
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346 | }
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347 |
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348 | // Transform Coordinates
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349 | ////////////////////////////////////////////////////////////////////////////
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350 | void bncRtnetDecoder::crdTrafo(int GPSWeek, ColumnVector& xyz,
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351 | const QString& trafo) {
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352 |
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353 | bnsSettings settings;
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354 |
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355 | if (trafo == "ETRF2000") {
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356 | _dx = 0.0541;
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357 | _dy = 0.0502;
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358 | _dz = -0.0538;
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359 | _dxr = -0.0002;
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360 | _dyr = 0.0001;
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361 | _dzr = -0.0018;
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362 | _ox = 0.000891;
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363 | _oy = 0.005390;
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364 | _oz = -0.008712;
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365 | _oxr = 0.000081;
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366 | _oyr = 0.000490;
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367 | _ozr = -0.000792;
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368 | _sc = 0.40;
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369 | _scr = 0.08;
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370 | _t0 = 2000.0;
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371 | }
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372 | else if (trafo == "NAD83") {
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373 | _dx = 0.9963;
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374 | _dy = -1.9024;
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375 | _dz = -0.5210;
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376 | _dxr = 0.0005;
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377 | _dyr = -0.0006;
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378 | _dzr = -0.0013;
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379 | _ox = 0.025915;
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380 | _oy = 0.009426;
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381 | _oz = 0.011599;
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382 | _oxr = 0.000067;
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383 | _oyr = -0.000757;
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384 | _ozr = -0.000051;
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385 | _sc = 0.78;
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386 | _scr = -0.10;
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387 | _t0 = 1997.0;
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388 | }
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389 | else if (trafo == "GDA94") {
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390 | _dx = -0.07973;
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391 | _dy = -0.00686;
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392 | _dz = 0.03803;
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393 | _dxr = 0.00225;
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394 | _dyr = -0.00062;
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395 | _dzr = -0.00056;
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396 | _ox = 0.0000351;
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397 | _oy = -0.0021211;
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398 | _oz = -0.0021411;
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399 | _oxr = -0.0014707;
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400 | _oyr = -0.0011443;
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401 | _ozr = -0.0011701;
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402 | _sc = 6.636;
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403 | _scr = 0.294;
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404 | _t0 = 1994.0;
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405 | }
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406 | else if (trafo == "SIRGAS2000") {
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407 | _dx = -0.0051;
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408 | _dy = -0.0065;
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409 | _dz = -0.0099;
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410 | _dxr = 0.0000;
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411 | _dyr = 0.0000;
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412 | _dzr = 0.0000;
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413 | _ox = 0.000150;
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414 | _oy = 0.000020;
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415 | _oz = 0.000021;
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416 | _oxr = 0.000000;
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417 | _oyr = 0.000000;
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418 | _ozr = 0.000000;
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419 | _sc = 0.000;
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420 | _scr = 0.000;
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421 | _t0 = 0000.0;
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422 | }
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423 | else if (trafo == "SIRGAS95") {
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424 | _dx = 0.0077;
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425 | _dy = 0.0058;
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426 | _dz = -0.0138;
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427 | _dxr = 0.0000;
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428 | _dyr = 0.0000;
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429 | _dzr = 0.0000;
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430 | _ox = 0.000000;
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431 | _oy = 0.000000;
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432 | _oz = -0.000030;
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433 | _oxr = 0.000000;
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434 | _oyr = 0.000000;
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435 | _ozr = 0.000000;
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436 | _sc = 1.570;
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437 | _scr = 0.000;
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438 | _t0 = 0000.0;
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439 | }
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440 | else if (trafo == "Custom") {
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441 | _dx = settings.value("trafo_dx").toDouble();
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442 | _dy = settings.value("trafo_dy").toDouble();
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443 | _dz = settings.value("trafo_dz").toDouble();
|
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444 | _dxr = settings.value("trafo_dxr").toDouble();
|
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445 | _dyr = settings.value("trafo_dyr").toDouble();
|
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446 | _dzr = settings.value("trafo_dzr").toDouble();
|
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447 | _ox = settings.value("trafo_ox").toDouble();
|
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448 | _oy = settings.value("trafo_oy").toDouble();
|
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449 | _oz = settings.value("trafo_oz").toDouble();
|
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450 | _oxr = settings.value("trafo_oxr").toDouble();
|
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451 | _oyr = settings.value("trafo_oyr").toDouble();
|
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452 | _ozr = settings.value("trafo_ozr").toDouble();
|
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453 | _sc = settings.value("trafo_sc").toDouble();
|
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454 | _scr = settings.value("trafo_scr").toDouble();
|
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455 | _t0 = settings.value("trafo_t0").toDouble();
|
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456 | }
|
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457 |
|
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458 | // Current epoch minus 2000.0 in years
|
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459 | // ------------------------------------
|
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460 | double dt = (GPSWeek - (1042.0+6.0/7.0)) / 365.2422 * 7.0 + 2000.0 - _t0;
|
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461 |
|
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462 | ColumnVector dx(3);
|
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463 |
|
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464 | dx(1) = _dx + dt * _dxr;
|
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465 | dx(2) = _dy + dt * _dyr;
|
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466 | dx(3) = _dz + dt * _dzr;
|
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467 |
|
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468 | static const double arcSec = 180.0 * 3600.0 / M_PI;
|
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469 |
|
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470 | double ox = (_ox + dt * _oxr) / arcSec;
|
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471 | double oy = (_oy + dt * _oyr) / arcSec;
|
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472 | double oz = (_oz + dt * _ozr) / arcSec;
|
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473 |
|
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474 | double sc = 1.0 + _sc * 1e-9 + dt * _scr * 1e-9;
|
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475 |
|
---|
476 | Matrix rMat(3,3);
|
---|
477 | rMat(1,1) = 1.0;
|
---|
478 | rMat(1,2) = -oz;
|
---|
479 | rMat(1,3) = oy;
|
---|
480 | rMat(2,1) = oz;
|
---|
481 | rMat(2,2) = 1.0;
|
---|
482 | rMat(2,3) = -ox;
|
---|
483 | rMat(3,1) = -oy;
|
---|
484 | rMat(3,2) = ox;
|
---|
485 | rMat(3,3) = 1.0;
|
---|
486 |
|
---|
487 | xyz = sc * rMat * xyz + dx;
|
---|
488 | }
|
---|