Changeset 7203 in ntrip for trunk/BNC/src
- Timestamp:
- Aug 17, 2015, 12:30:54 PM (9 years ago)
- Location:
- trunk/BNC/src
- Files:
-
- 15 added
- 5 edited
Legend:
- Unmodified
- Added
- Removed
-
trunk/BNC/src/PPP/pppClient.cpp
r6653 r7203 1 // Part of BNC, a utility for retrieving decoding and 2 // converting GNSS data streams from NTRIP broadcasters. 3 // 4 // Copyright (C) 2007 5 // German Federal Agency for Cartography and Geodesy (BKG) 6 // http://www.bkg.bund.de 7 // Czech Technical University Prague, Department of Geodesy 8 // http://www.fsv.cvut.cz 9 // 10 // Email: euref-ip@bkg.bund.de 11 // 12 // This program is free software; you can redistribute it and/or 13 // modify it under the terms of the GNU General Public License 14 // as published by the Free Software Foundation, version 2. 15 // 16 // This program is distributed in the hope that it will be useful, 17 // but WITHOUT ANY WARRANTY; without even the implied warranty of 18 // MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the 19 // GNU General Public License for more details. 20 // 21 // You should have received a copy of the GNU General Public License 22 // along with this program; if not, write to the Free Software 23 // Foundation, Inc., 59 Temple Place - Suite 330, Boston, MA 02111-1307, USA. 24 1 25 /* ------------------------------------------------------------------------- 2 26 * BKG NTRIP Client … … 5 29 * Class: t_pppClient 6 30 * 7 * Purpose: P PP Client processing starts here31 * Purpose: Precise Point Positioning 8 32 * 9 33 * Author: L. Mervart 10 34 * 11 * Created: 2 9-Jul-201435 * Created: 21-Nov-2009 12 36 * 13 37 * Changes: … … 15 39 * -----------------------------------------------------------------------*/ 16 40 17 #include <QThreadStorage> 18 19 #include <iostream> 41 #include <newmatio.h> 20 42 #include <iomanip> 21 #include <stdlib.h> 22 #include <string.h> 23 #include <stdexcept> 43 #include <sstream> 24 44 25 45 #include "pppClient.h" 26 #include "pppEphPool.h" 27 #include "pppObsPool.h" 28 #include "bncconst.h" 46 #include "bncephuser.h" 29 47 #include "bncutils.h" 30 #include "pppStation.h"31 #include "bncantex.h"32 #include "pppFilter.h"33 48 34 49 using namespace BNC_PPP; 35 50 using namespace std; 36 51 37 // Global variable holding thread-specific pointers 52 // Constructor 53 //////////////////////////////////////////////////////////////////////////// 54 t_pppClient::t_pppClient(const t_pppOptions* opt) { 55 56 _opt = new t_pppOptions(*opt); 57 _filter = new t_pppFilter(this); 58 _epoData = new t_epoData(); 59 _log = new ostringstream(); 60 _ephUser = new bncEphUser(false); 61 62 for (unsigned ii = 0; ii <= t_prn::MAXPRN; ii++) { 63 _satCodeBiases[ii] = 0; 64 } 65 66 } 67 68 // Destructor 69 //////////////////////////////////////////////////////////////////////////// 70 t_pppClient::~t_pppClient() { 71 72 for (unsigned ii = 0; ii <= t_prn::MAXPRN; ii++) { 73 delete _satCodeBiases[ii]; 74 } 75 76 delete _filter; 77 delete _epoData; 78 delete _opt; 79 delete _ephUser; 80 delete _log; 81 } 82 83 // 84 //////////////////////////////////////////////////////////////////////////// 85 void t_pppClient::processEpoch(const vector<t_satObs*>& satObs, t_output* output) { 86 87 // Convert and store observations 88 // ------------------------------ 89 _epoData->clear(); 90 for (unsigned ii = 0; ii < satObs.size(); ii++) { 91 const t_satObs* obs = satObs[ii]; 92 t_prn prn = obs->_prn; 93 if (prn.system() == 'E') {prn.setFlags(1);} // force I/NAV usage 94 t_satData* satData = new t_satData(); 95 96 if (_epoData->tt.undef()) { 97 _epoData->tt = obs->_time; 98 } 99 100 satData->tt = obs->_time; 101 satData->prn = QString(prn.toInternalString().c_str()); 102 satData->slipFlag = false; 103 satData->P1 = 0.0; 104 satData->P2 = 0.0; 105 satData->P5 = 0.0; 106 satData->P7 = 0.0; 107 satData->L1 = 0.0; 108 satData->L2 = 0.0; 109 satData->L5 = 0.0; 110 satData->L7 = 0.0; 111 for (unsigned ifrq = 0; ifrq < obs->_obs.size(); ifrq++) { 112 t_frqObs* frqObs = obs->_obs[ifrq]; 113 double cb = 0.0; 114 const t_satCodeBias* satCB = satCodeBias(prn); 115 if (satCB && satCB->_bias.size()) { 116 for (unsigned ii = 0; ii < satCB->_bias.size(); ii++) { 117 118 const t_frqCodeBias& bias = satCB->_bias[ii]; 119 if (frqObs && frqObs->_rnxType2ch == bias._rnxType2ch) { 120 cb = bias._value; 121 } 122 } 123 } 124 if (frqObs->_rnxType2ch[0] == '1') { 125 if (frqObs->_codeValid) satData->P1 = frqObs->_code + cb; 126 if (frqObs->_phaseValid) satData->L1 = frqObs->_phase; 127 if (frqObs->_slip) satData->slipFlag = true; 128 } 129 else if (frqObs->_rnxType2ch[0] == '2') { 130 if (frqObs->_codeValid) satData->P2 = frqObs->_code + cb; 131 if (frqObs->_phaseValid) satData->L2 = frqObs->_phase; 132 if (frqObs->_slip) satData->slipFlag = true; 133 } 134 else if (frqObs->_rnxType2ch[0] == '5') { 135 if (frqObs->_codeValid) satData->P5 = frqObs->_code + cb; 136 if (frqObs->_phaseValid) satData->L5 = frqObs->_phase; 137 if (frqObs->_slip) satData->slipFlag = true; 138 } 139 else if (frqObs->_rnxType2ch[0] == '7') { 140 if (frqObs->_codeValid) satData->P7 = frqObs->_code + cb; 141 if (frqObs->_phaseValid) satData->L7 = frqObs->_phase; 142 if (frqObs->_slip) satData->slipFlag = true; 143 } 144 } 145 putNewObs(satData); 146 } 147 148 // Data Pre-Processing 149 // ------------------- 150 QMutableMapIterator<QString, t_satData*> it(_epoData->satData); 151 while (it.hasNext()) { 152 it.next(); 153 QString prn = it.key(); 154 t_satData* satData = it.value(); 155 156 if (cmpToT(satData) != success) { 157 delete satData; 158 it.remove(); 159 continue; 160 } 161 162 } 163 164 // Filter Solution 165 // --------------- 166 if (_filter->update(_epoData) == success) { 167 output->_error = false; 168 output->_epoTime = _filter->time(); 169 output->_xyzRover[0] = _filter->x(); 170 output->_xyzRover[1] = _filter->y(); 171 output->_xyzRover[2] = _filter->z(); 172 copy(&_filter->Q().data()[0], &_filter->Q().data()[6], output->_covMatrix); 173 output->_neu[0] = _filter->neu()[0]; 174 output->_neu[1] = _filter->neu()[1]; 175 output->_neu[2] = _filter->neu()[2]; 176 output->_numSat = _filter->numSat(); 177 output->_pDop = _filter->PDOP(); 178 output->_trp0 = _filter->trp0(); 179 output->_trp = _filter->trp(); 180 } 181 else { 182 output->_error = true; 183 } 184 185 output->_log = _log->str(); 186 delete _log; _log = new ostringstream(); 187 } 188 189 // 190 //////////////////////////////////////////////////////////////////////////// 191 void t_pppClient::putNewObs(t_satData* satData) { 192 193 // Set Observations GPS 194 // -------------------- 195 if (satData->system() == 'G') { 196 if (satData->P1 != 0.0 && satData->P2 != 0.0 && 197 satData->L1 != 0.0 && satData->L2 != 0.0 ) { 198 t_frequency::type fType1 = t_lc::toFreq(satData->system(), t_lc::l1); 199 t_frequency::type fType2 = t_lc::toFreq(satData->system(), t_lc::l2); 200 double f1 = t_CST::freq(fType1, 0); 201 double f2 = t_CST::freq(fType2, 0); 202 double a1 = f1 * f1 / (f1 * f1 - f2 * f2); 203 double a2 = - f2 * f2 / (f1 * f1 - f2 * f2); 204 satData->L1 = satData->L1 * t_CST::c / f1; 205 satData->L2 = satData->L2 * t_CST::c / f2; 206 satData->P3 = a1 * satData->P1 + a2 * satData->P2; 207 satData->L3 = a1 * satData->L1 + a2 * satData->L2; 208 satData->lambda3 = a1 * t_CST::c / f1 + a2 * t_CST::c / f2; 209 satData->lkA = a1; 210 satData->lkB = a2; 211 _epoData->satData[satData->prn] = satData; 212 } 213 else { 214 delete satData; 215 } 216 } 217 218 // Set Observations Glonass 219 // ------------------------ 220 else if (satData->system() == 'R' && _opt->useSystem('R')) { 221 if (satData->P1 != 0.0 && satData->P2 != 0.0 && 222 satData->L1 != 0.0 && satData->L2 != 0.0 ) { 223 224 int channel = 0; 225 if (satData->system() == 'R') { 226 const t_eph* eph = _ephUser->ephLast(satData->prn); 227 if (eph) { 228 channel = eph->slotNum(); 229 } 230 else { 231 delete satData; 232 return; 233 } 234 } 235 236 t_frequency::type fType1 = t_lc::toFreq(satData->system(), t_lc::l1); 237 t_frequency::type fType2 = t_lc::toFreq(satData->system(), t_lc::l2); 238 double f1 = t_CST::freq(fType1, channel); 239 double f2 = t_CST::freq(fType2, channel); 240 double a1 = f1 * f1 / (f1 * f1 - f2 * f2); 241 double a2 = - f2 * f2 / (f1 * f1 - f2 * f2); 242 satData->L1 = satData->L1 * t_CST::c / f1; 243 satData->L2 = satData->L2 * t_CST::c / f2; 244 satData->P3 = a1 * satData->P1 + a2 * satData->P2; 245 satData->L3 = a1 * satData->L1 + a2 * satData->L2; 246 satData->lambda3 = a1 * t_CST::c / f1 + a2 * t_CST::c / f2; 247 satData->lkA = a1; 248 satData->lkB = a2; 249 _epoData->satData[satData->prn] = satData; 250 } 251 else { 252 delete satData; 253 } 254 } 255 256 // Set Observations Galileo 257 // ------------------------ 258 else if (satData->system() == 'E' && _opt->useSystem('E')) { 259 if (satData->P1 != 0.0 && satData->P5 != 0.0 && 260 satData->L1 != 0.0 && satData->L5 != 0.0 ) { 261 double f1 = t_CST::freq(t_frequency::E1, 0); 262 double f5 = t_CST::freq(t_frequency::E5, 0); 263 double a1 = f1 * f1 / (f1 * f1 - f5 * f5); 264 double a5 = - f5 * f5 / (f1 * f1 - f5 * f5); 265 satData->L1 = satData->L1 * t_CST::c / f1; 266 satData->L5 = satData->L5 * t_CST::c / f5; 267 satData->P3 = a1 * satData->P1 + a5 * satData->P5; 268 satData->L3 = a1 * satData->L1 + a5 * satData->L5; 269 satData->lambda3 = a1 * t_CST::c / f1 + a5 * t_CST::c / f5; 270 satData->lkA = a1; 271 satData->lkB = a5; 272 _epoData->satData[satData->prn] = satData; 273 } 274 else { 275 delete satData; 276 } 277 } 278 279 // Set Observations BDS 280 // --------------------- 281 else if (satData->system() == 'C' && _opt->useSystem('C')) { 282 if (satData->P2 != 0.0 && satData->P7 != 0.0 && 283 satData->L2 != 0.0 && satData->L7 != 0.0 ) { 284 double f2 = t_CST::freq(t_frequency::C2, 0); 285 double f7 = t_CST::freq(t_frequency::C7, 0); 286 double a2 = f2 * f2 / (f2 * f2 - f7 * f7); 287 double a7 = - f7 * f7 / (f2 * f2 - f7 * f7); 288 satData->L2 = satData->L2 * t_CST::c / f2; 289 satData->L7 = satData->L7 * t_CST::c / f7; 290 satData->P3 = a2 * satData->P2 + a7 * satData->P7; 291 satData->L3 = a2 * satData->L2 + a7 * satData->L7; 292 satData->lambda3 = a2 * t_CST::c / f2 + a7 * t_CST::c / f7; 293 satData->lkA = a2; 294 satData->lkB = a7; 295 _epoData->satData[satData->prn] = satData; 296 } 297 else { 298 delete satData; 299 } 300 } 301 } 302 303 // 304 //////////////////////////////////////////////////////////////////////////// 305 void t_pppClient::putOrbCorrections(const std::vector<t_orbCorr*>& corr) { 306 for (unsigned ii = 0; ii < corr.size(); ii++) { 307 QString prn = QString(corr[ii]->_prn.toInternalString().c_str()); 308 t_eph* eLast = _ephUser->ephLast(prn); 309 t_eph* ePrev = _ephUser->ephPrev(prn); 310 if (eLast && eLast->IOD() == corr[ii]->_iod) { 311 eLast->setOrbCorr(corr[ii]); 312 } 313 else if (ePrev && ePrev->IOD() == corr[ii]->_iod) { 314 ePrev->setOrbCorr(corr[ii]); 315 } 316 } 317 } 318 319 // 320 //////////////////////////////////////////////////////////////////////////// 321 void t_pppClient::putClkCorrections(const std::vector<t_clkCorr*>& corr) { 322 for (unsigned ii = 0; ii < corr.size(); ii++) { 323 QString prn = QString(corr[ii]->_prn.toInternalString().c_str()); 324 t_eph* eLast = _ephUser->ephLast(prn); 325 t_eph* ePrev = _ephUser->ephPrev(prn); 326 if (eLast && eLast->IOD() == corr[ii]->_iod) { 327 eLast->setClkCorr(corr[ii]); 328 } 329 else if (ePrev && ePrev->IOD() == corr[ii]->_iod) { 330 ePrev->setClkCorr(corr[ii]); 331 } 332 } 333 } 334 335 // 38 336 ////////////////////////////////////////////////////////////////////////////// 39 QThreadStorage<t_pppClient*> CLIENTS; 40 41 // Static function returning thread-specific pointer 42 ////////////////////////////////////////////////////////////////////////////// 43 t_pppClient* t_pppClient::instance() { 44 return CLIENTS.localData(); 45 } 46 47 // Constructor 48 ////////////////////////////////////////////////////////////////////////////// 49 t_pppClient::t_pppClient(const t_pppOptions* opt) { 50 _output = 0; 51 _opt = new t_pppOptions(*opt); 52 _log = new ostringstream(); 53 _ephPool = new t_pppEphPool(); 54 _obsPool = new t_pppObsPool(); 55 _staRover = new t_pppStation(); 56 _filter = new t_pppFilter(); 57 _tides = new t_tides(); 58 59 if (!_opt->_antexFileName.empty()) { 60 _antex = new bncAntex(_opt->_antexFileName.c_str()); 61 } 62 else { 63 _antex = 0; 64 } 65 66 CLIENTS.setLocalData(this); // CLIENTS takes ownership over "this" 67 } 68 69 // Destructor 70 ////////////////////////////////////////////////////////////////////////////// 71 t_pppClient::~t_pppClient() { 72 delete _log; 73 delete _opt; 74 delete _ephPool; 75 delete _obsPool; 76 delete _staRover; 77 delete _antex; 78 delete _filter; 79 delete _tides; 80 clearObs(); 337 void t_pppClient::putCodeBiases(const std::vector<t_satCodeBias*>& satCodeBias) { 338 for (unsigned ii = 0; ii < satCodeBias.size(); ii++) { 339 putCodeBias(new t_satCodeBias(*satCodeBias[ii])); 340 } 81 341 } 82 342 … … 84 344 ////////////////////////////////////////////////////////////////////////////// 85 345 void t_pppClient::putEphemeris(const t_eph* eph) { 346 bool check = _opt->_realTime; 86 347 const t_ephGPS* ephGPS = dynamic_cast<const t_ephGPS*>(eph); 87 348 const t_ephGlo* ephGlo = dynamic_cast<const t_ephGlo*>(eph); 88 349 const t_ephGal* ephGal = dynamic_cast<const t_ephGal*>(eph); 350 const t_ephBDS* ephBDS = dynamic_cast<const t_ephBDS*>(eph); 89 351 if (ephGPS) { 90 _eph Pool->putEphemeris(new t_ephGPS(*ephGPS));352 _ephUser->putNewEph(new t_ephGPS(*ephGPS), check); 91 353 } 92 354 else if (ephGlo) { 93 _eph Pool->putEphemeris(new t_ephGlo(*ephGlo));355 _ephUser->putNewEph(new t_ephGlo(*ephGlo), check); 94 356 } 95 357 else if (ephGal) { 96 _ephPool->putEphemeris(new t_ephGal(*ephGal)); 97 } 98 } 99 100 // 101 ////////////////////////////////////////////////////////////////////////////// 102 void t_pppClient::putOrbCorrections(const vector<t_orbCorr*>& corr) { 103 for (unsigned ii = 0; ii < corr.size(); ii++) { 104 _ephPool->putOrbCorrection(new t_orbCorr(*corr[ii])); 105 } 106 } 107 108 // 109 ////////////////////////////////////////////////////////////////////////////// 110 void t_pppClient::putClkCorrections(const vector<t_clkCorr*>& corr) { 111 for (unsigned ii = 0; ii < corr.size(); ii++) { 112 _ephPool->putClkCorrection(new t_clkCorr(*corr[ii])); 113 } 114 } 115 116 // 117 ////////////////////////////////////////////////////////////////////////////// 118 void t_pppClient::putCodeBiases(const vector<t_satCodeBias*>& biases) { 119 for (unsigned ii = 0; ii < biases.size(); ii++) { 120 _obsPool->putCodeBias(new t_satCodeBias(*biases[ii])); 121 } 122 } 123 124 // 125 ////////////////////////////////////////////////////////////////////////////// 126 t_irc t_pppClient::prepareObs(const vector<t_satObs*>& satObs, 127 vector<t_pppSatObs*>& obsVector, bncTime& epoTime) { 128 // Default 129 // ------- 130 epoTime.reset(); 131 132 // Create vector of valid observations 133 // ----------------------------------- 134 for (unsigned ii = 0; ii < satObs.size(); ii++) { 135 char system = satObs[ii]->_prn.system(); 136 if (OPT->useSystem(system)) { 137 t_pppSatObs* pppSatObs = new t_pppSatObs(*satObs[ii]); 138 if (pppSatObs->isValid()) { 139 obsVector.push_back(pppSatObs); 140 } 141 else { 142 delete pppSatObs; 143 } 144 } 145 } 146 147 // Check whether data are synchronized, compute epoTime 148 // ---------------------------------------------------- 149 const double MAXSYNC = 0.05; // synchronization limit 150 double meanDt = 0.0; 151 for (unsigned ii = 0; ii < obsVector.size(); ii++) { 152 const t_pppSatObs* satObs = obsVector.at(ii); 153 if (epoTime.undef()) { 154 epoTime = satObs->time(); 155 } 156 else { 157 double dt = satObs->time() - epoTime; 158 if (fabs(dt) > MAXSYNC) { 159 LOG << "t_pppClient::prepareObs asynchronous observations" << endl; 160 return failure; 161 } 162 meanDt += dt; 163 } 164 } 165 166 if (obsVector.size() > 0) { 167 epoTime += meanDt / obsVector.size(); 168 } 169 170 return success; 171 } 172 173 // Compute the Bancroft position, check for blunders 174 ////////////////////////////////////////////////////////////////////////////// 175 t_irc t_pppClient::cmpBancroft(const bncTime& epoTime, 176 vector<t_pppSatObs*>& obsVector, 177 ColumnVector& xyzc, bool print) { 178 179 t_lc::type tLC = t_lc::dummy; 180 181 while (true) { 182 Matrix BB(obsVector.size(), 4); 183 int iObs = -1; 184 for (unsigned ii = 0; ii < obsVector.size(); ii++) { 185 const t_pppSatObs* satObs = obsVector.at(ii); 186 if (satObs->prn().system() == 'G') { 187 if (tLC == t_lc::dummy) { 188 tLC = satObs->isValid(t_lc::cIF) ? t_lc::cIF : t_lc::c1; 189 } 190 if ( satObs->isValid(tLC) && (!satObs->modelSet() || satObs->eleSat() >= OPT->_minEle) ) { 191 ++iObs; 192 BB[iObs][0] = satObs->xc()[0]; 193 BB[iObs][1] = satObs->xc()[1]; 194 BB[iObs][2] = satObs->xc()[2]; 195 BB[iObs][3] = satObs->obsValue(tLC) - satObs->cmpValueForBanc(tLC); 196 } 197 } 198 } 199 if (iObs + 1 < OPT->_minObs) { 200 LOG << "t_pppClient::cmpBancroft not enough observations" << endl; 358 _ephUser->putNewEph(new t_ephGal(*ephGal), check); 359 } 360 else if (ephBDS) { 361 _ephUser->putNewEph(new t_ephBDS(*ephBDS), check); 362 } 363 } 364 365 // Satellite Position 366 //////////////////////////////////////////////////////////////////////////// 367 t_irc t_pppClient::getSatPos(const bncTime& tt, const QString& prn, 368 ColumnVector& xc, ColumnVector& vv) { 369 370 t_eph* eLast = _ephUser->ephLast(prn); 371 t_eph* ePrev = _ephUser->ephPrev(prn); 372 if (eLast && eLast->getCrd(tt, xc, vv, _opt->useOrbClkCorr()) == success) { 373 return success; 374 } 375 else if (ePrev && ePrev->getCrd(tt, xc, vv, _opt->useOrbClkCorr()) == success) { 376 return success; 377 } 378 return failure; 379 } 380 381 // Correct Time of Transmission 382 //////////////////////////////////////////////////////////////////////////// 383 t_irc t_pppClient::cmpToT(t_satData* satData) { 384 385 double prange = satData->P3; 386 if (prange == 0.0) { 387 return failure; 388 } 389 390 double clkSat = 0.0; 391 for (int ii = 1; ii <= 10; ii++) { 392 393 bncTime ToT = satData->tt - prange / t_CST::c - clkSat; 394 395 ColumnVector xc(4); 396 ColumnVector vv(3); 397 if (getSatPos(ToT, satData->prn, xc, vv) != success) { 201 398 return failure; 202 399 } 203 BB = BB.Rows(1,iObs+1); 204 bancroft(BB, xyzc); 205 206 xyzc[3] /= t_CST::c; 207 208 // Check Blunders 209 // -------------- 210 const double BLUNDER = 100.0; 211 double maxRes = 0.0; 212 unsigned maxResIndex = 0; 213 for (unsigned ii = 0; ii < obsVector.size(); ii++) { 214 const t_pppSatObs* satObs = obsVector.at(ii); 215 if ( satObs->isValid() && satObs->prn().system() == 'G' && 216 (!satObs->modelSet() || satObs->eleSat() >= OPT->_minEle) ) { 217 ColumnVector rr = satObs->xc().Rows(1,3) - xyzc.Rows(1,3); 218 double res = rr.norm_Frobenius() - satObs->obsValue(tLC) 219 - (satObs->xc()[3] - xyzc[3]) * t_CST::c; 220 if (fabs(res) > maxRes) { 221 maxRes = fabs(res); 222 maxResIndex = ii; 223 } 224 } 225 } 226 if (maxRes < BLUNDER) { 227 if (print) { 228 LOG.setf(ios::fixed); 229 LOG << string(epoTime) << " BANCROFT:" << ' ' 230 << setw(14) << setprecision(3) << xyzc[0] << ' ' 231 << setw(14) << setprecision(3) << xyzc[1] << ' ' 232 << setw(14) << setprecision(3) << xyzc[2] << ' ' 233 << setw(14) << setprecision(3) << xyzc[3] * t_CST::c << endl << endl; 234 } 235 break; 236 } 237 else { 238 t_pppSatObs* satObs = obsVector.at(maxResIndex); 239 LOG << "t_pppClient::cmpBancroft outlier " << satObs->prn().toString() 240 << " " << maxRes << endl; 241 delete satObs; 242 obsVector.erase(obsVector.begin() + maxResIndex); 243 } 244 } 245 246 return success; 247 } 248 249 // Compute A Priori GPS-Glonass Offset 250 ////////////////////////////////////////////////////////////////////////////// 251 double t_pppClient::cmpOffGG(vector<t_pppSatObs*>& obsVector) { 252 253 t_lc::type tLC = t_lc::dummy; 254 double offGG = 0.0; 255 256 if (OPT->useSystem('R')) { 257 258 while (obsVector.size() > 0) { 259 offGG = 0.0; 260 double maxRes = 0.0; 261 int maxResIndex = -1; 262 t_prn maxResPrn; 263 unsigned nObs = 0; 264 for (unsigned ii = 0; ii < obsVector.size(); ii++) { 265 t_pppSatObs* satObs = obsVector.at(ii); 266 if (satObs->prn().system() == 'R') { 267 if (tLC == t_lc::dummy) { 268 tLC = satObs->isValid(t_lc::cIF) ? t_lc::cIF : t_lc::c1; 269 } 270 if (satObs->isValid(tLC) && (!satObs->modelSet() || satObs->eleSat() >= OPT->_minEle)) { 271 double ll = satObs->obsValue(tLC) - satObs->cmpValue(tLC); 272 ++nObs; 273 offGG += ll; 274 if (fabs(ll) > fabs(maxRes)) { 275 maxRes = ll; 276 maxResIndex = ii; 277 maxResPrn = satObs->prn(); 278 } 279 } 280 } 281 } 282 283 if (nObs > 0) { 284 offGG = offGG / nObs; 285 } 286 else { 287 offGG = 0.0; 288 } 289 290 if (fabs(maxRes) > 1000.0) { 291 LOG << "t_pppClient::cmpOffGG outlier " << maxResPrn.toString() << " " << maxRes << endl; 292 obsVector.erase(obsVector.begin() + maxResIndex); 293 } 294 else { 295 break; 296 } 297 } 298 } 299 300 return offGG; 301 } 302 303 // 304 ////////////////////////////////////////////////////////////////////////////// 305 void t_pppClient::initOutput(t_output* output) { 306 _output = output; 307 _output->_numSat = 0; 308 _output->_pDop = 0.0; 309 _output->_error = false; 310 } 311 312 // 313 ////////////////////////////////////////////////////////////////////////////// 314 void t_pppClient::clearObs() { 315 for (unsigned ii = 0; ii < _obsRover.size(); ii++) { 316 delete _obsRover.at(ii); 317 } 318 _obsRover.clear(); 319 } 320 321 // 322 ////////////////////////////////////////////////////////////////////////////// 323 void t_pppClient::finish(t_irc irc) { 324 325 clearObs(); 326 327 _output->_epoTime = _epoTimeRover; 328 329 if (irc == success) { 330 _output->_xyzRover[0] = _staRover->xyzApr()[0] + _filter->x()[0]; 331 _output->_xyzRover[1] = _staRover->xyzApr()[1] + _filter->x()[1]; 332 _output->_xyzRover[2] = _staRover->xyzApr()[2] + _filter->x()[2]; 333 334 xyz2neu(_staRover->ellApr().data(), _filter->x().data(), _output->_neu); 335 336 copy(&_filter->Q().data()[0], &_filter->Q().data()[6], _output->_covMatrix); 337 338 _output->_trp0 = t_tropo::delay_saast(_staRover->xyzApr(), M_PI/2.0); 339 _output->_trp = _filter->trp(); 340 _output->_trpStdev = _filter->trpStdev(); 341 342 _output->_numSat = _filter->numSat(); 343 _output->_pDop = _filter->PDOP(); 344 _output->_error = false; 345 } 346 else { 347 _output->_error = true; 348 } 349 _output->_log = _log->str(); 350 delete _log; _log = new ostringstream(); 351 } 352 353 // 354 ////////////////////////////////////////////////////////////////////////////// 355 t_irc t_pppClient::cmpModel(t_pppStation* station, const ColumnVector& xyzc, 356 vector<t_pppSatObs*>& obsVector) { 357 358 bncTime time; 359 time = _epoTimeRover; 360 station->setName(OPT->_roverName); 361 station->setAntName(OPT->_antNameRover); 362 if (OPT->xyzAprRoverSet()) { 363 station->setXyzApr(OPT->_xyzAprRover); 364 } 365 else { 366 station->setXyzApr(xyzc.Rows(1,3)); 367 } 368 station->setNeuEcc(OPT->_neuEccRover); 369 370 // Receiver Clock 371 // -------------- 372 station->setDClk(xyzc[3]); 373 374 // Tides 375 // ----- 376 station->setTideDspl( _tides->displacement(time, station->xyzApr()) ); 377 378 // Observation model 379 // ----------------- 380 vector<t_pppSatObs*>::iterator it = obsVector.begin(); 381 while (it != obsVector.end()) { 382 t_pppSatObs* satObs = *it; 383 if (satObs->isValid()) { 384 satObs->cmpModel(station); 385 } 386 if (satObs->isValid() && satObs->eleSat() >= OPT->_minEle) { 387 ++it; 388 } 389 else { 390 delete satObs; 391 it = obsVector.erase(it); 392 } 393 } 394 395 return success; 396 } 397 398 // 399 ////////////////////////////////////////////////////////////////////////////// 400 void t_pppClient::processEpoch(const vector<t_satObs*>& satObs, t_output* output) { 401 402 try { 403 initOutput(output); 404 405 // Prepare Observations of the Rover 406 // --------------------------------- 407 if (prepareObs(satObs, _obsRover, _epoTimeRover) != success) { 408 return finish(failure); 409 } 410 411 LOG << "\nResults of Epoch "; 412 if (!_epoTimeRover.undef()) LOG << string(_epoTimeRover); 413 LOG << "\n--------------------------------------\n"; 414 415 for (int iter = 1; iter <= 2; iter++) { 416 ColumnVector xyzc(4); xyzc = 0.0; 417 bool print = (iter == 2); 418 if (cmpBancroft(_epoTimeRover, _obsRover, xyzc, print) != success) { 419 return finish(failure); 420 } 421 if (cmpModel(_staRover, xyzc, _obsRover) != success) { 422 return finish(failure); 423 } 424 } 425 426 _offGG = cmpOffGG(_obsRover); 427 428 // Store last epoch of data 429 // ------------------------ 430 _obsPool->putEpoch(_epoTimeRover, _obsRover); 431 432 // Process Epoch in Filter 433 // ----------------------- 434 if (_filter->processEpoch(_obsPool) != success) { 435 return finish(failure); 436 } 437 } 438 catch (Exception& exc) { 439 LOG << exc.what() << endl; 440 return finish(failure); 441 } 442 catch (t_except msg) { 443 LOG << msg.what() << endl; 444 return finish(failure); 445 } 446 catch (const char* msg) { 447 LOG << msg << endl; 448 return finish(failure); 449 } 450 catch (...) { 451 LOG << "unknown exception" << endl; 452 return finish(failure); 453 } 454 455 return finish(success); 456 } 457 458 // 459 //////////////////////////////////////////////////////////////////////////// 460 double lorentz(const ColumnVector& aa, const ColumnVector& bb) { 461 return aa[0]*bb[0] + aa[1]*bb[1] + aa[2]*bb[2] - aa[3]*bb[3]; 462 } 463 464 // 465 //////////////////////////////////////////////////////////////////////////// 466 void t_pppClient::bancroft(const Matrix& BBpass, ColumnVector& pos) { 467 468 if (pos.Nrows() != 4) { 469 pos.ReSize(4); 470 } 471 pos = 0.0; 472 473 for (int iter = 1; iter <= 2; iter++) { 474 Matrix BB = BBpass; 475 int mm = BB.Nrows(); 476 for (int ii = 1; ii <= mm; ii++) { 477 double xx = BB(ii,1); 478 double yy = BB(ii,2); 479 double traveltime = 0.072; 480 if (iter > 1) { 481 double zz = BB(ii,3); 482 double rho = sqrt( (xx-pos(1)) * (xx-pos(1)) + 483 (yy-pos(2)) * (yy-pos(2)) + 484 (zz-pos(3)) * (zz-pos(3)) ); 485 traveltime = rho / t_CST::c; 486 } 487 double angle = traveltime * t_CST::omega; 488 double cosa = cos(angle); 489 double sina = sin(angle); 490 BB(ii,1) = cosa * xx + sina * yy; 491 BB(ii,2) = -sina * xx + cosa * yy; 492 } 493 494 Matrix BBB; 495 if (mm > 4) { 496 SymmetricMatrix hlp; hlp << BB.t() * BB; 497 BBB = hlp.i() * BB.t(); 498 } 499 else { 500 BBB = BB.i(); 501 } 502 ColumnVector ee(mm); ee = 1.0; 503 ColumnVector alpha(mm); alpha = 0.0; 504 for (int ii = 1; ii <= mm; ii++) { 505 alpha(ii) = lorentz(BB.Row(ii).t(),BB.Row(ii).t())/2.0; 506 } 507 ColumnVector BBBe = BBB * ee; 508 ColumnVector BBBalpha = BBB * alpha; 509 double aa = lorentz(BBBe, BBBe); 510 double bb = lorentz(BBBe, BBBalpha)-1; 511 double cc = lorentz(BBBalpha, BBBalpha); 512 double root = sqrt(bb*bb-aa*cc); 513 514 Matrix hlpPos(4,2); 515 hlpPos.Column(1) = (-bb-root)/aa * BBBe + BBBalpha; 516 hlpPos.Column(2) = (-bb+root)/aa * BBBe + BBBalpha; 517 518 ColumnVector omc(2); 519 for (int pp = 1; pp <= 2; pp++) { 520 hlpPos(4,pp) = -hlpPos(4,pp); 521 omc(pp) = BB(1,4) - 522 sqrt( (BB(1,1)-hlpPos(1,pp)) * (BB(1,1)-hlpPos(1,pp)) + 523 (BB(1,2)-hlpPos(2,pp)) * (BB(1,2)-hlpPos(2,pp)) + 524 (BB(1,3)-hlpPos(3,pp)) * (BB(1,3)-hlpPos(3,pp)) ) - 525 hlpPos(4,pp); 526 } 527 if ( fabs(omc(1)) > fabs(omc(2)) ) { 528 pos = hlpPos.Column(2); 529 } 530 else { 531 pos = hlpPos.Column(1); 532 } 533 } 534 } 535 400 401 double clkSatOld = clkSat; 402 clkSat = xc(4); 403 404 if ( fabs(clkSat-clkSatOld) * t_CST::c < 1.e-4 ) { 405 satData->xx = xc.Rows(1,3); 406 satData->vv = vv; 407 satData->clk = clkSat * t_CST::c; 408 return success; 409 } 410 } 411 412 return failure; 413 } 414 415 void t_pppClient::putCodeBias(t_satCodeBias* satCodeBias) { 416 int iPrn = satCodeBias->_prn.toInt(); 417 delete _satCodeBiases[iPrn]; 418 _satCodeBiases[iPrn] = satCodeBias; 419 } -
trunk/BNC/src/PPP/pppClient.h
r6463 r7203 1 // Part of BNC, a utility for retrieving decoding and 2 // converting GNSS data streams from NTRIP broadcasters. 3 // 4 // Copyright (C) 2007 5 // German Federal Agency for Cartography and Geodesy (BKG) 6 // http://www.bkg.bund.de 7 // Czech Technical University Prague, Department of Geodesy 8 // http://www.fsv.cvut.cz 9 // 10 // Email: euref-ip@bkg.bund.de 11 // 12 // This program is free software; you can redistribute it and/or 13 // modify it under the terms of the GNU General Public License 14 // as published by the Free Software Foundation, version 2. 15 // 16 // This program is distributed in the hope that it will be useful, 17 // but WITHOUT ANY WARRANTY; without even the implied warranty of 18 // MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the 19 // GNU General Public License for more details. 20 // 21 // You should have received a copy of the GNU General Public License 22 // along with this program; if not, write to the Free Software 23 // Foundation, Inc., 59 Temple Place - Suite 330, Boston, MA 02111-1307, USA. 24 1 25 #ifndef PPPCLIENT_H 2 26 #define PPPCLIENT_H 3 27 4 #include <sstream>5 28 #include <vector> 29 #include <QtCore> 30 6 31 #include "pppInclude.h" 7 #include "ephemeris.h"8 32 #include "pppOptions.h" 9 #include "pppModel.h" 10 #include "satObs.h" 33 #include "pppFilter.h" 11 34 12 class bncAntex; 35 class bncEphUser; 36 class t_eph; 13 37 14 38 namespace BNC_PPP { 15 16 class t_pppEphPool; 17 class t_pppObsPool; 18 class t_pppSatObs; 19 class t_pppStation; 20 class t_pppFilter; 21 39 22 40 class t_pppClient : public interface_pppClient { 23 41 public: 24 t_pppClient(const t_pppOptions* opt); 25 ~t_pppClient(); 42 t_pppClient(const t_pppOptions* opt); 43 ~t_pppClient(); 44 void processEpoch(const std::vector<t_satObs*>& satObs, t_output* output); 45 void putEphemeris(const t_eph* eph); 46 void putOrbCorrections(const std::vector<t_orbCorr*>& corr); 47 void putClkCorrections(const std::vector<t_clkCorr*>& corr); 48 void putCodeBiases(const std::vector<t_satCodeBias*>& satCodeBias); 49 std::ostringstream& log() {return *_log;} 50 const t_pppOptions* opt() const {return _opt;} 51 void putCodeBias(t_satCodeBias* satCodeBias); 52 const t_satCodeBias* satCodeBias(const t_prn& prn) const { 53 return _satCodeBiases[prn.toInt()]; 54 } 55 private: 56 t_irc getSatPos(const bncTime& tt, const QString& prn, ColumnVector& xc, ColumnVector& vv); 57 void putNewObs(t_satData* satData); 58 t_irc cmpToT(t_satData* satData); 26 59 27 void putEphemeris(const t_eph* eph); 28 void putOrbCorrections(const std::vector<t_orbCorr*>& corr); 29 void putClkCorrections(const std::vector<t_clkCorr*>& corr); 30 void putCodeBiases(const std::vector<t_satCodeBias*>& satBias); 31 void processEpoch(const std::vector<t_satObs*>& satObs, t_output* output); 32 33 const t_pppEphPool* ephPool() const {return _ephPool;} 34 const t_pppObsPool* obsPool() const {return _obsPool;} 35 const bncAntex* antex() const {return _antex;} 36 const t_pppStation* staRover() const {return _staRover;} 37 double offGG() const {return _offGG;} 38 39 std::ostringstream& log() {return *_log;} 40 const t_pppOptions* opt() const {return _opt;} 41 42 static void bancroft(const Matrix& BBpass, ColumnVector& pos); 43 44 static t_pppClient* instance(); 45 46 private: 47 void initOutput(t_output* output); 48 void finish(t_irc irc); 49 void clearObs(); 50 t_irc prepareObs(const std::vector<t_satObs*>& satObs, 51 std::vector<t_pppSatObs*>& obsVector, bncTime& epoTime); 52 t_irc cmpModel(t_pppStation* station, const ColumnVector& xyzc, 53 std::vector<t_pppSatObs*>& obsVector); 54 t_irc cmpBancroft(const bncTime& epoTime, std::vector<t_pppSatObs*>& obsVector, 55 ColumnVector& xyzc, bool print); 56 double cmpOffGG(std::vector<t_pppSatObs*>& obsVector); 57 58 t_output* _output; 59 t_pppEphPool* _ephPool; 60 t_pppObsPool* _obsPool; 61 bncTime _epoTimeRover; 62 t_pppStation* _staRover; 63 bncAntex* _antex; 64 t_pppFilter* _filter; 65 double _offGG; 66 std::vector<t_pppSatObs*> _obsRover; 67 std::ostringstream* _log; 68 t_pppOptions* _opt; 69 t_tides* _tides; 60 t_satCodeBias* _satCodeBiases[t_prn::MAXPRN+1]; 61 bncEphUser* _ephUser; 62 t_pppOptions* _opt; 63 t_epoData* _epoData; 64 t_pppFilter* _filter; 65 std::ostringstream* _log; 70 66 }; 71 67 72 }; // namespace BNC_PPP 73 74 #define PPP_CLIENT (BNC_PPP::t_pppClient::instance()) 75 #define LOG (BNC_PPP::t_pppClient::instance()->log()) 76 #define OPT (BNC_PPP::t_pppClient::instance()->opt()) 68 } // namespace 77 69 78 70 #endif -
trunk/BNC/src/PPP/pppFilter.cpp
r6997 r7203 1 // Part of BNC, a utility for retrieving decoding and 2 // converting GNSS data streams from NTRIP broadcasters. 3 // 4 // Copyright (C) 2007 5 // German Federal Agency for Cartography and Geodesy (BKG) 6 // http://www.bkg.bund.de 7 // Czech Technical University Prague, Department of Geodesy 8 // http://www.fsv.cvut.cz 9 // 10 // Email: euref-ip@bkg.bund.de 11 // 12 // This program is free software; you can redistribute it and/or 13 // modify it under the terms of the GNU General Public License 14 // as published by the Free Software Foundation, version 2. 15 // 16 // This program is distributed in the hope that it will be useful, 17 // but WITHOUT ANY WARRANTY; without even the implied warranty of 18 // MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the 19 // GNU General Public License for more details. 20 // 21 // You should have received a copy of the GNU General Public License 22 // along with this program; if not, write to the Free Software 23 // Foundation, Inc., 59 Temple Place - Suite 330, Boston, MA 02111-1307, USA. 24 1 25 /* ------------------------------------------------------------------------- 2 26 * BKG NTRIP Client 3 27 * ------------------------------------------------------------------------- 4 28 * 5 * Class: t_ppp Filter29 * Class: t_pppParam, t_pppFilter 6 30 * 7 * Purpose: Filter Adjustment31 * Purpose: Model for PPP 8 32 * 9 33 * Author: L. Mervart 10 34 * 11 * Created: 29-Jul-201435 * Created: 01-Dec-2009 12 36 * 13 37 * Changes: … … 15 39 * -----------------------------------------------------------------------*/ 16 40 17 #include <iostream>18 41 #include <iomanip> 19 42 #include <cmath> 20 #include < newmat.h>43 #include <sstream> 21 44 #include <newmatio.h> 22 45 #include <newmatap.h> 23 46 24 47 #include "pppFilter.h" 48 #include "pppClient.h" 25 49 #include "bncutils.h" 26 #include "pppParlist.h" 27 #include "pppObsPool.h" 28 #include "pppStation.h" 29 #include "pppClient.h" 50 #include "bncantex.h" 51 #include "pppOptions.h" 52 #include "pppModel.h" 30 53 31 54 using namespace BNC_PPP; 32 55 using namespace std; 33 56 57 const double MAXRES_CODE = 2.98 * 3.0; 58 const double MAXRES_PHASE_GPS = 2.98 * 0.03; 59 const double MAXRES_PHASE_GLONASS = 2.98 * 0.03; 60 const double GLONASS_WEIGHT_FACTOR = 1.0; 61 const double BDS_WEIGHT_FACTOR = 2.0; 62 63 #define LOG (_pppClient->log()) 64 #define OPT (_pppClient->opt()) 65 34 66 // Constructor 35 67 //////////////////////////////////////////////////////////////////////////// 36 t_pppFilter::t_pppFilter() { 37 _parlist = 0; 68 t_pppParam::t_pppParam(t_pppParam::parType typeIn, int indexIn, 69 const QString& prnIn) { 70 type = typeIn; 71 index = indexIn; 72 prn = prnIn; 73 index_old = 0; 74 xx = 0.0; 75 numEpo = 0; 38 76 } 39 77 40 78 // Destructor 41 79 //////////////////////////////////////////////////////////////////////////// 80 t_pppParam::~t_pppParam() { 81 } 82 83 // Partial 84 //////////////////////////////////////////////////////////////////////////// 85 double t_pppParam::partial(t_satData* satData, bool phase) { 86 87 Tracer tracer("t_pppParam::partial"); 88 89 // Coordinates 90 // ----------- 91 if (type == CRD_X) { 92 return (xx - satData->xx(1)) / satData->rho; 93 } 94 else if (type == CRD_Y) { 95 return (xx - satData->xx(2)) / satData->rho; 96 } 97 else if (type == CRD_Z) { 98 return (xx - satData->xx(3)) / satData->rho; 99 } 100 101 // Receiver Clocks 102 // --------------- 103 else if (type == RECCLK) { 104 return 1.0; 105 } 106 107 // Troposphere 108 // ----------- 109 else if (type == TROPO) { 110 return 1.0 / sin(satData->eleSat); 111 } 112 113 // Glonass Offset 114 // -------------- 115 else if (type == GLONASS_OFFSET) { 116 if (satData->prn[0] == 'R') { 117 return 1.0; 118 } 119 else { 120 return 0.0; 121 } 122 } 123 124 // Galileo Offset 125 // -------------- 126 else if (type == GALILEO_OFFSET) { 127 if (satData->prn[0] == 'E') { 128 return 1.0; 129 } 130 else { 131 return 0.0; 132 } 133 } 134 135 // BDS Offset 136 // ---------- 137 else if (type == BDS_OFFSET) { 138 if (satData->prn[0] == 'C') { 139 return 1.0; 140 } 141 else { 142 return 0.0; 143 } 144 } 145 146 // Ambiguities 147 // ----------- 148 else if (type == AMB_L3) { 149 if (phase && satData->prn == prn) { 150 return 1.0; 151 } 152 else { 153 return 0.0; 154 } 155 } 156 157 // Default return 158 // -------------- 159 return 0.0; 160 } 161 162 // Constructor 163 //////////////////////////////////////////////////////////////////////////// 164 t_pppFilter::t_pppFilter(t_pppClient* pppClient) { 165 166 _pppClient = pppClient; 167 _tides = new t_tides(); 168 169 // Antenna Name, ANTEX File 170 // ------------------------ 171 _antex = 0; 172 if (!OPT->_antexFileName.empty()) { 173 _antex = new bncAntex(OPT->_antexFileName.c_str()); 174 } 175 176 // Bancroft Coordinates 177 // -------------------- 178 _xcBanc.ReSize(4); _xcBanc = 0.0; 179 _ellBanc.ReSize(3); _ellBanc = 0.0; 180 181 // Save copy of data (used in outlier detection) 182 // --------------------------------------------- 183 _epoData_sav = new t_epoData(); 184 185 // Some statistics 186 // --------------- 187 _neu.ReSize(3); _neu = 0.0; 188 _numSat = 0; 189 _pDop = 0.0; 190 } 191 192 // Destructor 193 //////////////////////////////////////////////////////////////////////////// 42 194 t_pppFilter::~t_pppFilter() { 43 delete _parlist; 44 } 45 46 // Process Single Epoch 47 //////////////////////////////////////////////////////////////////////////// 48 t_irc t_pppFilter::processEpoch(t_pppObsPool* obsPool) { 49 50 _numSat = 0; 51 52 if (!_parlist) { 53 _parlist = new t_pppParlist(); 54 } 55 56 // Vector of all Observations 57 // -------------------------- 58 t_pppObsPool::t_epoch* epoch = obsPool->lastEpoch(); 59 if (!epoch) { 195 delete _tides; 196 delete _antex; 197 for (int iPar = 1; iPar <= _params.size(); iPar++) { 198 delete _params[iPar-1]; 199 } 200 for (int iPar = 1; iPar <= _params_sav.size(); iPar++) { 201 delete _params_sav[iPar-1]; 202 } 203 delete _epoData_sav; 204 } 205 206 // Reset Parameters and Variance-Covariance Matrix 207 //////////////////////////////////////////////////////////////////////////// 208 void t_pppFilter::reset() { 209 210 Tracer tracer("t_pppFilter::reset"); 211 212 double lastTrp = 0.0; 213 for (int ii = 0; ii < _params.size(); ii++) { 214 t_pppParam* pp = _params[ii]; 215 if (pp->type == t_pppParam::TROPO) { 216 lastTrp = pp->xx; 217 } 218 delete pp; 219 } 220 _params.clear(); 221 222 int nextPar = 0; 223 _params.push_back(new t_pppParam(t_pppParam::CRD_X, ++nextPar, "")); 224 _params.push_back(new t_pppParam(t_pppParam::CRD_Y, ++nextPar, "")); 225 _params.push_back(new t_pppParam(t_pppParam::CRD_Z, ++nextPar, "")); 226 _params.push_back(new t_pppParam(t_pppParam::RECCLK, ++nextPar, "")); 227 if (OPT->estTrp()) { 228 _params.push_back(new t_pppParam(t_pppParam::TROPO, ++nextPar, "")); 229 } 230 if (OPT->useSystem('R')) { 231 _params.push_back(new t_pppParam(t_pppParam::GLONASS_OFFSET, ++nextPar, "")); 232 } 233 if (OPT->useSystem('E')) { 234 _params.push_back(new t_pppParam(t_pppParam::GALILEO_OFFSET, ++nextPar, "")); 235 } 236 if (OPT->useSystem('C')) { 237 _params.push_back(new t_pppParam(t_pppParam::BDS_OFFSET, ++nextPar, "")); 238 } 239 240 _QQ.ReSize(_params.size()); 241 _QQ = 0.0; 242 for (int iPar = 1; iPar <= _params.size(); iPar++) { 243 t_pppParam* pp = _params[iPar-1]; 244 pp->xx = 0.0; 245 if (pp->isCrd()) { 246 _QQ(iPar,iPar) = OPT->_aprSigCrd(1) * OPT->_aprSigCrd(1); 247 } 248 else if (pp->type == t_pppParam::RECCLK) { 249 _QQ(iPar,iPar) = OPT->_noiseClk * OPT->_noiseClk; 250 } 251 else if (pp->type == t_pppParam::TROPO) { 252 _QQ(iPar,iPar) = OPT->_aprSigTrp * OPT->_aprSigTrp; 253 pp->xx = lastTrp; 254 } 255 else if (pp->type == t_pppParam::GLONASS_OFFSET) { 256 _QQ(iPar,iPar) = 1000.0 * 1000.0; 257 } 258 else if (pp->type == t_pppParam::GALILEO_OFFSET) { 259 _QQ(iPar,iPar) = 1000.0 * 1000.0; 260 } 261 else if (pp->type == t_pppParam::BDS_OFFSET) { 262 _QQ(iPar,iPar) = 1000.0 * 1000.0; 263 } 264 } 265 } 266 267 // Bancroft Solution 268 //////////////////////////////////////////////////////////////////////////// 269 t_irc t_pppFilter::cmpBancroft(t_epoData* epoData) { 270 271 Tracer tracer("t_pppFilter::cmpBancroft"); 272 273 if (int(epoData->sizeSys('G')) < OPT->_minObs) { 274 LOG << "t_pppFilter::cmpBancroft: not enough data\n"; 60 275 return failure; 61 276 } 62 vector<t_pppSatObs*>& allObs = epoch->obsVector(); 63 64 // Time of the Epoch 65 // ----------------- 66 _epoTime = epoch->epoTime(); 67 68 if (!_firstEpoTime.valid()) { 69 _firstEpoTime = _epoTime; 70 } 71 72 // Set Parameters 73 // -------------- 74 _parlist->set(_epoTime, allObs); 75 const vector<t_pppParam*>& params = _parlist->params(); 76 77 // Status Vector, Variance-Covariance Matrix 78 // ----------------------------------------- 79 ColumnVector xFltOld = _xFlt; 80 SymmetricMatrix QFltOld = _QFlt; 81 82 _QFlt.ReSize(_parlist->nPar()); _QFlt = 0.0; 83 _xFlt.ReSize(_parlist->nPar()); _xFlt = 0.0; 84 _x0.ReSize(_parlist->nPar()); _x0 = 0.0; 277 278 Matrix BB(epoData->sizeSys('G'), 4); 279 280 QMapIterator<QString, t_satData*> it(epoData->satData); 281 int iObsBanc = 0; 282 while (it.hasNext()) { 283 it.next(); 284 t_satData* satData = it.value(); 285 if (satData->system() == 'G') { 286 ++iObsBanc; 287 QString prn = it.key(); 288 BB(iObsBanc, 1) = satData->xx(1); 289 BB(iObsBanc, 2) = satData->xx(2); 290 BB(iObsBanc, 3) = satData->xx(3); 291 BB(iObsBanc, 4) = satData->P3 + satData->clk; 292 } 293 } 294 295 bancroft(BB, _xcBanc); 296 297 // Ellipsoidal Coordinates 298 // ------------------------ 299 xyz2ell(_xcBanc.data(), _ellBanc.data()); 300 301 // Compute Satellite Elevations 302 // ---------------------------- 303 QMutableMapIterator<QString, t_satData*> im(epoData->satData); 304 while (im.hasNext()) { 305 im.next(); 306 t_satData* satData = im.value(); 307 cmpEle(satData); 308 if (satData->eleSat < OPT->_minEle) { 309 delete satData; 310 im.remove(); 311 } 312 } 313 314 return success; 315 } 316 317 // Computed Value 318 //////////////////////////////////////////////////////////////////////////// 319 double t_pppFilter::cmpValue(t_satData* satData, bool phase) { 320 321 Tracer tracer("t_pppFilter::cmpValue"); 322 323 ColumnVector xRec(3); 324 xRec(1) = x(); 325 xRec(2) = y(); 326 xRec(3) = z(); 327 328 double rho0 = (satData->xx - xRec).norm_Frobenius(); 329 double dPhi = t_CST::omega * rho0 / t_CST::c; 330 331 xRec(1) = x() * cos(dPhi) - y() * sin(dPhi); 332 xRec(2) = y() * cos(dPhi) + x() * sin(dPhi); 333 xRec(3) = z(); 334 335 xRec += _tides->displacement(_time, xRec); 336 337 satData->rho = (satData->xx - xRec).norm_Frobenius(); 338 339 double tropDelay = delay_saast(satData->eleSat) + 340 trp() / sin(satData->eleSat); 341 342 double wind = 0.0; 343 if (phase) { 344 wind = windUp(satData->prn, satData->xx, xRec) * satData->lambda3; 345 } 346 347 double offset = 0.0; 348 t_frequency::type frqA = t_frequency::G1; 349 t_frequency::type frqB = t_frequency::G2; 350 if (satData->prn[0] == 'R') { 351 offset = Glonass_offset(); 352 frqA = t_frequency::R1; 353 frqB = t_frequency::R2; 354 } 355 else if (satData->prn[0] == 'E') { 356 offset = Galileo_offset(); 357 //frqA = t_frequency::E1; as soon as available 358 //frqB = t_frequency::E5; -"- 359 } 360 else if (satData->prn[0] == 'C') { 361 offset = Bds_offset(); 362 //frqA = t_frequency::C2; as soon as available 363 //frqB = t_frequency::C7; -"- 364 } 365 double phaseCenter = 0.0; 366 if (_antex) { 367 bool found; 368 phaseCenter = satData->lkA * _antex->rcvCorr(OPT->_antNameRover, frqA, 369 satData->eleSat, satData->azSat, 370 found) 371 + satData->lkB * _antex->rcvCorr(OPT->_antNameRover, frqB, 372 satData->eleSat, satData->azSat, 373 found); 374 if (!found) { 375 LOG << "ANTEX: antenna >" << OPT->_antNameRover << "< not found\n"; 376 } 377 } 378 379 double antennaOffset = 0.0; 380 double cosa = cos(satData->azSat); 381 double sina = sin(satData->azSat); 382 double cose = cos(satData->eleSat); 383 double sine = sin(satData->eleSat); 384 antennaOffset = -OPT->_neuEccRover(1) * cosa*cose 385 -OPT->_neuEccRover(2) * sina*cose 386 -OPT->_neuEccRover(3) * sine; 387 388 return satData->rho + phaseCenter + antennaOffset + clk() 389 + offset - satData->clk + tropDelay + wind; 390 } 391 392 // Tropospheric Model (Saastamoinen) 393 //////////////////////////////////////////////////////////////////////////// 394 double t_pppFilter::delay_saast(double Ele) { 395 396 Tracer tracer("t_pppFilter::delay_saast"); 397 398 double xyz[3]; 399 xyz[0] = x(); 400 xyz[1] = y(); 401 xyz[2] = z(); 402 double ell[3]; 403 xyz2ell(xyz, ell); 404 double height = ell[2]; 405 406 double pp = 1013.25 * pow(1.0 - 2.26e-5 * height, 5.225); 407 double TT = 18.0 - height * 0.0065 + 273.15; 408 double hh = 50.0 * exp(-6.396e-4 * height); 409 double ee = hh / 100.0 * exp(-37.2465 + 0.213166*TT - 0.000256908*TT*TT); 410 411 double h_km = height / 1000.0; 85 412 86 for (unsigned ii = 0; ii < params.size(); ii++) { 87 const t_pppParam* par1 = params[ii]; 88 89 _x0[ii] = par1->x0(); 90 91 int iOld = par1->indexOld(); 92 if (iOld < 0) { 93 _QFlt[ii][ii] = par1->sigma0() * par1->sigma0(); // new parameter 94 } 95 else { 96 _QFlt[ii][ii] = QFltOld[iOld][iOld] + par1->noise() * par1->noise(); 97 _xFlt[ii] = xFltOld[iOld]; 98 for (unsigned jj = 0; jj < ii; jj++) { 99 const t_pppParam* par2 = params[jj]; 100 int jOld = par2->indexOld(); 101 if (jOld >= 0) { 102 _QFlt[ii][jj] = QFltOld(iOld+1,jOld+1); 413 if (h_km < 0.0) h_km = 0.0; 414 if (h_km > 5.0) h_km = 5.0; 415 int ii = int(h_km + 1); 416 double href = ii - 1; 417 418 double bCor[6]; 419 bCor[0] = 1.156; 420 bCor[1] = 1.006; 421 bCor[2] = 0.874; 422 bCor[3] = 0.757; 423 bCor[4] = 0.654; 424 bCor[5] = 0.563; 425 426 double BB = bCor[ii-1] + (bCor[ii]-bCor[ii-1]) * (h_km - href); 427 428 double zen = M_PI/2.0 - Ele; 429 430 return (0.002277/cos(zen)) * (pp + ((1255.0/TT)+0.05)*ee - BB*(tan(zen)*tan(zen))); 431 } 432 433 // Prediction Step of the Filter 434 //////////////////////////////////////////////////////////////////////////// 435 void t_pppFilter::predict(int iPhase, t_epoData* epoData) { 436 437 Tracer tracer("t_pppFilter::predict"); 438 439 if (iPhase == 0) { 440 441 const double maxSolGap = 60.0; 442 443 bool firstCrd = false; 444 if (!_lastTimeOK.valid() || (maxSolGap > 0.0 && _time - _lastTimeOK > maxSolGap)) { 445 firstCrd = true; 446 _startTime = epoData->tt; 447 reset(); 448 } 449 450 // Use different white noise for Quick-Start mode 451 // ---------------------------------------------- 452 double sigCrdP_used = OPT->_noiseCrd(1); 453 if ( OPT->_seedingTime > 0.0 && OPT->_seedingTime > (epoData->tt - _startTime) ) { 454 sigCrdP_used = 0.0; 455 } 456 457 // Predict Parameter values, add white noise 458 // ----------------------------------------- 459 for (int iPar = 1; iPar <= _params.size(); iPar++) { 460 t_pppParam* pp = _params[iPar-1]; 461 462 // Coordinates 463 // ----------- 464 if (pp->type == t_pppParam::CRD_X) { 465 if (firstCrd) { 466 if (OPT->xyzAprRoverSet()) { 467 pp->xx = OPT->_xyzAprRover[0]; 468 } 469 else { 470 pp->xx = _xcBanc(1); 471 } 103 472 } 104 } 105 } 106 } 107 108 predictCovCrdPart(QFltOld); 109 110 // Process Satellite Systems separately 111 // ------------------------------------ 112 for (unsigned iSys = 0; iSys < OPT->systems().size(); iSys++) { 113 char system = OPT->systems()[iSys]; 114 vector<t_pppSatObs*> obsVector; 115 for (unsigned jj = 0; jj < allObs.size(); jj++) { 116 if (allObs[jj]->prn().system() == system) { 117 obsVector.push_back(allObs[jj]); 118 } 119 } 120 if ( processSystem(OPT->LCs(system), obsVector) != success ) { 121 return failure; 122 } 123 } 124 125 cmpDOP(allObs); 126 127 _parlist->printResult(_epoTime, _QFlt, _xFlt); 128 129 return success; 130 } 131 132 // Process Selected LCs 133 //////////////////////////////////////////////////////////////////////////// 134 t_irc t_pppFilter::processSystem(const vector<t_lc::type>& LCs, 135 const vector<t_pppSatObs*>& obsVector) { 136 137 LOG.setf(ios::fixed); 138 139 // Detect Cycle Slips 140 // ------------------ 141 if (detectCycleSlips(LCs, obsVector) != success) { 142 return failure; 143 } 144 145 ColumnVector xSav = _xFlt; 146 SymmetricMatrix QSav = _QFlt; 147 string epoTimeStr = string(_epoTime); 148 const vector<t_pppParam*>& params = _parlist->params(); 149 unsigned maxObs = obsVector.size() * LCs.size(); 150 473 _QQ(iPar,iPar) += sigCrdP_used * sigCrdP_used; 474 } 475 else if (pp->type == t_pppParam::CRD_Y) { 476 if (firstCrd) { 477 if (OPT->xyzAprRoverSet()) { 478 pp->xx = OPT->_xyzAprRover[1]; 479 } 480 else { 481 pp->xx = _xcBanc(2); 482 } 483 } 484 _QQ(iPar,iPar) += sigCrdP_used * sigCrdP_used; 485 } 486 else if (pp->type == t_pppParam::CRD_Z) { 487 if (firstCrd) { 488 if (OPT->xyzAprRoverSet()) { 489 pp->xx = OPT->_xyzAprRover[2]; 490 } 491 else { 492 pp->xx = _xcBanc(3); 493 } 494 } 495 _QQ(iPar,iPar) += sigCrdP_used * sigCrdP_used; 496 } 497 498 // Receiver Clocks 499 // --------------- 500 else if (pp->type == t_pppParam::RECCLK) { 501 pp->xx = _xcBanc(4); 502 for (int jj = 1; jj <= _params.size(); jj++) { 503 _QQ(iPar, jj) = 0.0; 504 } 505 _QQ(iPar,iPar) = OPT->_noiseClk * OPT->_noiseClk; 506 } 507 508 // Tropospheric Delay 509 // ------------------ 510 else if (pp->type == t_pppParam::TROPO) { 511 _QQ(iPar,iPar) += OPT->_noiseTrp * OPT->_noiseTrp; 512 } 513 514 // Glonass Offset 515 // -------------- 516 else if (pp->type == t_pppParam::GLONASS_OFFSET) { 517 pp->xx = 0.0; 518 for (int jj = 1; jj <= _params.size(); jj++) { 519 _QQ(iPar, jj) = 0.0; 520 } 521 _QQ(iPar,iPar) = 1000.0 * 1000.0; 522 } 523 524 // Galileo Offset 525 // -------------- 526 else if (pp->type == t_pppParam::GALILEO_OFFSET) { 527 _QQ(iPar,iPar) += 0.1 * 0.1; 528 } 529 530 // BDS Offset 531 // ---------- 532 else if (pp->type == t_pppParam::BDS_OFFSET) { 533 _QQ(iPar,iPar) = 1000.0 * 1000.0; //TODO: TEST 534 } 535 } 536 } 537 538 // Add New Ambiguities if necessary 539 // -------------------------------- 540 if (OPT->ambLCs('G').size() || OPT->ambLCs('R').size() || 541 OPT->ambLCs('E').size() || OPT->ambLCs('C').size()) { 542 543 // Make a copy of QQ and xx, set parameter indices 544 // ----------------------------------------------- 545 SymmetricMatrix QQ_old = _QQ; 546 547 for (int iPar = 1; iPar <= _params.size(); iPar++) { 548 _params[iPar-1]->index_old = _params[iPar-1]->index; 549 _params[iPar-1]->index = 0; 550 } 551 552 // Remove Ambiguity Parameters without observations 553 // ------------------------------------------------ 554 int iPar = 0; 555 QMutableVectorIterator<t_pppParam*> im(_params); 556 while (im.hasNext()) { 557 t_pppParam* par = im.next(); 558 bool removed = false; 559 if (par->type == t_pppParam::AMB_L3) { 560 if (epoData->satData.find(par->prn) == epoData->satData.end()) { 561 removed = true; 562 delete par; 563 im.remove(); 564 } 565 } 566 if (! removed) { 567 ++iPar; 568 par->index = iPar; 569 } 570 } 571 572 // Add new ambiguity parameters 573 // ---------------------------- 574 QMapIterator<QString, t_satData*> it(epoData->satData); 575 while (it.hasNext()) { 576 it.next(); 577 t_satData* satData = it.value(); 578 addAmb(satData); 579 } 580 581 int nPar = _params.size(); 582 _QQ.ReSize(nPar); _QQ = 0.0; 583 for (int i1 = 1; i1 <= nPar; i1++) { 584 t_pppParam* p1 = _params[i1-1]; 585 if (p1->index_old != 0) { 586 _QQ(p1->index, p1->index) = QQ_old(p1->index_old, p1->index_old); 587 for (int i2 = 1; i2 <= nPar; i2++) { 588 t_pppParam* p2 = _params[i2-1]; 589 if (p2->index_old != 0) { 590 _QQ(p1->index, p2->index) = QQ_old(p1->index_old, p2->index_old); 591 } 592 } 593 } 594 } 595 596 for (int ii = 1; ii <= nPar; ii++) { 597 t_pppParam* par = _params[ii-1]; 598 if (par->index_old == 0) { 599 _QQ(par->index, par->index) = OPT->_aprSigAmb * OPT->_aprSigAmb; 600 } 601 par->index_old = par->index; 602 } 603 } 604 } 605 606 // Update Step of the Filter (currently just a single-epoch solution) 607 //////////////////////////////////////////////////////////////////////////// 608 t_irc t_pppFilter::update(t_epoData* epoData) { 609 610 Tracer tracer("t_pppFilter::update"); 611 612 _time = epoData->tt; // current epoch time 613 614 if (OPT->useOrbClkCorr()) { 615 LOG << "Precise Point Positioning of Epoch " << _time.datestr() << "_" << _time.timestr(1) 616 << "\n---------------------------------------------------------------\n"; 617 } 618 else { 619 LOG << "Single Point Positioning of Epoch " << _time.datestr() << "_" << _time.timestr(1) 620 << "\n--------------------------------------------------------------\n"; 621 } 622 151 623 // Outlier Detection Loop 152 624 // ---------------------- 153 for (unsigned iOutlier = 0; iOutlier < maxObs; iOutlier++) { 154 155 if (iOutlier > 0) { 156 _xFlt = xSav; 157 _QFlt = QSav; 158 } 159 160 // First-Design Matrix, Terms Observed-Computed, Weight Matrix 161 // ----------------------------------------------------------- 162 Matrix AA(maxObs, _parlist->nPar()); 163 ColumnVector ll(maxObs); 164 DiagonalMatrix PP(maxObs); PP = 0.0; 165 166 int iObs = -1; 167 vector<t_pppSatObs*> usedObs; 168 vector<t_lc::type> usedTypes; 169 for (unsigned ii = 0; ii < obsVector.size(); ii++) { 170 t_pppSatObs* obs = obsVector[ii]; 171 if (!obs->outlier()) { 172 for (unsigned jj = 0; jj < LCs.size(); jj++) { 173 const t_lc::type tLC = LCs[jj]; 174 ++iObs; 175 usedObs.push_back(obs); 176 usedTypes.push_back(tLC); 177 for (unsigned iPar = 0; iPar < params.size(); iPar++) { 178 const t_pppParam* par = params[iPar]; 179 AA[iObs][iPar] = par->partial(_epoTime, obs, tLC); 625 if (update_p(epoData) != success) { 626 return failure; 627 } 628 629 // Set Solution Vector 630 // ------------------- 631 LOG.setf(ios::fixed); 632 QVectorIterator<t_pppParam*> itPar(_params); 633 while (itPar.hasNext()) { 634 t_pppParam* par = itPar.next(); 635 if (par->type == t_pppParam::RECCLK) { 636 LOG << "\n clk = " << setw(10) << setprecision(3) << par->xx 637 << " +- " << setw(6) << setprecision(3) 638 << sqrt(_QQ(par->index,par->index)); 639 } 640 else if (par->type == t_pppParam::AMB_L3) { 641 ++par->numEpo; 642 LOG << "\n amb " << par->prn.mid(0,3).toAscii().data() << " = " 643 << setw(10) << setprecision(3) << par->xx 644 << " +- " << setw(6) << setprecision(3) 645 << sqrt(_QQ(par->index,par->index)) 646 << " nEpo = " << par->numEpo; 647 } 648 else if (par->type == t_pppParam::TROPO) { 649 double aprTrp = delay_saast(M_PI/2.0); 650 LOG << "\n trp = " << par->prn.mid(0,3).toAscii().data() 651 << setw(7) << setprecision(3) << aprTrp << " " 652 << setw(6) << setprecision(3) << showpos << par->xx << noshowpos 653 << " +- " << setw(6) << setprecision(3) 654 << sqrt(_QQ(par->index,par->index)); 655 } 656 else if (par->type == t_pppParam::GLONASS_OFFSET) { 657 LOG << "\n offGlo = " << setw(10) << setprecision(3) << par->xx 658 << " +- " << setw(6) << setprecision(3) 659 << sqrt(_QQ(par->index,par->index)); 660 } 661 else if (par->type == t_pppParam::GALILEO_OFFSET) { 662 LOG << "\n offGal = " << setw(10) << setprecision(3) << par->xx 663 << " +- " << setw(6) << setprecision(3) 664 << sqrt(_QQ(par->index,par->index)); 665 } 666 else if (par->type == t_pppParam::BDS_OFFSET) { 667 LOG << "\n offBds = " << setw(10) << setprecision(3) << par->xx 668 << " +- " << setw(6) << setprecision(3) 669 << sqrt(_QQ(par->index,par->index)); 670 } 671 } 672 673 LOG << endl << endl; 674 675 // Compute dilution of precision 676 // ----------------------------- 677 cmpDOP(epoData); 678 679 // Final Message (both log file and screen) 680 // ---------------------------------------- 681 LOG << OPT->_roverName << " PPP " 682 << epoData->tt.timestr(1) << " " << epoData->sizeAll() << " " 683 << setw(14) << setprecision(3) << x() << " +- " 684 << setw(6) << setprecision(3) << sqrt(_QQ(1,1)) << " " 685 << setw(14) << setprecision(3) << y() << " +- " 686 << setw(6) << setprecision(3) << sqrt(_QQ(2,2)) << " " 687 << setw(14) << setprecision(3) << z() << " +- " 688 << setw(6) << setprecision(3) << sqrt(_QQ(3,3)); 689 690 // NEU Output 691 // ---------- 692 if (OPT->xyzAprRoverSet()) { 693 double xyz[3]; 694 xyz[0] = x() - OPT->_xyzAprRover[0]; 695 xyz[1] = y() - OPT->_xyzAprRover[1]; 696 xyz[2] = z() - OPT->_xyzAprRover[2]; 697 698 double ellRef[3]; 699 xyz2ell(OPT->_xyzAprRover.data(), ellRef); 700 xyz2neu(ellRef, xyz, _neu.data()); 701 702 LOG << " NEU " 703 << setw(8) << setprecision(3) << _neu[0] << " " 704 << setw(8) << setprecision(3) << _neu[1] << " " 705 << setw(8) << setprecision(3) << _neu[2] << endl << endl; 706 } 707 else { 708 LOG << endl << endl; 709 } 710 711 _lastTimeOK = _time; // remember time of last successful update 712 return success; 713 } 714 715 // Outlier Detection 716 //////////////////////////////////////////////////////////////////////////// 717 QString t_pppFilter::outlierDetection(int iPhase, const ColumnVector& vv, 718 QMap<QString, t_satData*>& satData) { 719 720 Tracer tracer("t_pppFilter::outlierDetection"); 721 722 QString prnGPS; 723 QString prnGlo; 724 double maxResGPS = 0.0; // all the other systems except GLONASS 725 double maxResGlo = 0.0; // GLONASS 726 findMaxRes(vv, satData, prnGPS, prnGlo, maxResGPS, maxResGlo); 727 728 if (iPhase == 1) { 729 if (maxResGlo > 2.98 * OPT->_maxResL1) { 730 LOG << "Outlier Phase " << prnGlo.mid(0,3).toAscii().data() << ' ' << maxResGlo << endl; 731 return prnGlo; 732 } 733 else if (maxResGPS > 2.98 * OPT->_maxResL1) { 734 LOG << "Outlier Phase " << prnGPS.mid(0,3).toAscii().data() << ' ' << maxResGPS << endl; 735 return prnGPS; 736 } 737 } 738 else if (iPhase == 0 && maxResGPS > 2.98 * OPT->_maxResC1) { 739 LOG << "Outlier Code " << prnGPS.mid(0,3).toAscii().data() << ' ' << maxResGPS << endl; 740 return prnGPS; 741 } 742 743 return QString(); 744 } 745 746 // Phase Wind-Up Correction 747 /////////////////////////////////////////////////////////////////////////// 748 double t_pppFilter::windUp(const QString& prn, const ColumnVector& rSat, 749 const ColumnVector& rRec) { 750 751 Tracer tracer("t_pppFilter::windUp"); 752 753 double Mjd = _time.mjd() + _time.daysec() / 86400.0; 754 755 // First time - initialize to zero 756 // ------------------------------- 757 if (!_windUpTime.contains(prn)) { 758 _windUpSum[prn] = 0.0; 759 } 760 761 // Compute the correction for new time 762 // ----------------------------------- 763 if (!_windUpTime.contains(prn) || _windUpTime[prn] != Mjd) { 764 _windUpTime[prn] = Mjd; 765 766 // Unit Vector GPS Satellite --> Receiver 767 // -------------------------------------- 768 ColumnVector rho = rRec - rSat; 769 rho /= rho.norm_Frobenius(); 770 771 // GPS Satellite unit Vectors sz, sy, sx 772 // ------------------------------------- 773 ColumnVector sz = -rSat / rSat.norm_Frobenius(); 774 775 ColumnVector xSun = t_astro::Sun(Mjd); 776 xSun /= xSun.norm_Frobenius(); 777 778 ColumnVector sy = crossproduct(sz, xSun); 779 ColumnVector sx = crossproduct(sy, sz); 780 781 // Effective Dipole of the GPS Satellite Antenna 782 // --------------------------------------------- 783 ColumnVector dipSat = sx - rho * DotProduct(rho,sx) 784 - crossproduct(rho, sy); 785 786 // Receiver unit Vectors rx, ry 787 // ---------------------------- 788 ColumnVector rx(3); 789 ColumnVector ry(3); 790 791 double recEll[3]; xyz2ell(rRec.data(), recEll) ; 792 double neu[3]; 793 794 neu[0] = 1.0; 795 neu[1] = 0.0; 796 neu[2] = 0.0; 797 neu2xyz(recEll, neu, rx.data()); 798 799 neu[0] = 0.0; 800 neu[1] = -1.0; 801 neu[2] = 0.0; 802 neu2xyz(recEll, neu, ry.data()); 803 804 // Effective Dipole of the Receiver Antenna 805 // ---------------------------------------- 806 ColumnVector dipRec = rx - rho * DotProduct(rho,rx) 807 + crossproduct(rho, ry); 808 809 // Resulting Effect 810 // ---------------- 811 double alpha = DotProduct(dipSat,dipRec) / 812 (dipSat.norm_Frobenius() * dipRec.norm_Frobenius()); 813 814 if (alpha > 1.0) alpha = 1.0; 815 if (alpha < -1.0) alpha = -1.0; 816 817 double dphi = acos(alpha) / 2.0 / M_PI; // in cycles 818 819 if ( DotProduct(rho, crossproduct(dipSat, dipRec)) < 0.0 ) { 820 dphi = -dphi; 821 } 822 823 _windUpSum[prn] = floor(_windUpSum[prn] - dphi + 0.5) + dphi; 824 } 825 826 return _windUpSum[prn]; 827 } 828 829 // 830 /////////////////////////////////////////////////////////////////////////// 831 void t_pppFilter::cmpEle(t_satData* satData) { 832 Tracer tracer("t_pppFilter::cmpEle"); 833 ColumnVector rr = satData->xx - _xcBanc.Rows(1,3); 834 double rho = rr.norm_Frobenius(); 835 836 double neu[3]; 837 xyz2neu(_ellBanc.data(), rr.data(), neu); 838 839 satData->eleSat = acos( sqrt(neu[0]*neu[0] + neu[1]*neu[1]) / rho ); 840 if (neu[2] < 0) { 841 satData->eleSat *= -1.0; 842 } 843 satData->azSat = atan2(neu[1], neu[0]); 844 } 845 846 // 847 /////////////////////////////////////////////////////////////////////////// 848 void t_pppFilter::addAmb(t_satData* satData) { 849 Tracer tracer("t_pppFilter::addAmb"); 850 if (!OPT->ambLCs(satData->system()).size()){ 851 return; 852 } 853 bool found = false; 854 for (int iPar = 1; iPar <= _params.size(); iPar++) { 855 if (_params[iPar-1]->type == t_pppParam::AMB_L3 && 856 _params[iPar-1]->prn == satData->prn) { 857 found = true; 858 break; 859 } 860 } 861 if (!found) { 862 t_pppParam* par = new t_pppParam(t_pppParam::AMB_L3, 863 _params.size()+1, satData->prn); 864 _params.push_back(par); 865 par->xx = satData->L3 - cmpValue(satData, true); 866 } 867 } 868 869 // 870 /////////////////////////////////////////////////////////////////////////// 871 void t_pppFilter::addObs(int iPhase, unsigned& iObs, t_satData* satData, 872 Matrix& AA, ColumnVector& ll, DiagonalMatrix& PP) { 873 874 Tracer tracer("t_pppFilter::addObs"); 875 876 const double ELEWGHT = 20.0; 877 double ellWgtCoef = 1.0; 878 double eleD = satData->eleSat * 180.0 / M_PI; 879 if (eleD < ELEWGHT) { 880 ellWgtCoef = 1.5 - 0.5 / (ELEWGHT - 10.0) * (eleD - 10.0); 881 } 882 883 // Remember Observation Index 884 // -------------------------- 885 ++iObs; 886 satData->obsIndex = iObs; 887 888 // Phase Observations 889 // ------------------ 890 891 if (iPhase == 1) { 892 ll(iObs) = satData->L3 - cmpValue(satData, true); 893 double sigL3 = 2.98 * OPT->_sigmaL1; 894 if (satData->system() == 'R') { 895 sigL3 *= GLONASS_WEIGHT_FACTOR; 896 } 897 if (satData->system() == 'C') { 898 sigL3 *= BDS_WEIGHT_FACTOR; 899 } 900 PP(iObs,iObs) = 1.0 / (sigL3 * sigL3) / (ellWgtCoef * ellWgtCoef); 901 for (int iPar = 1; iPar <= _params.size(); iPar++) { 902 if (_params[iPar-1]->type == t_pppParam::AMB_L3 && 903 _params[iPar-1]->prn == satData->prn) { 904 ll(iObs) -= _params[iPar-1]->xx; 905 } 906 AA(iObs, iPar) = _params[iPar-1]->partial(satData, true); 907 } 908 } 909 910 // Code Observations 911 // ----------------- 912 else { 913 double sigP3 = 2.98 * OPT->_sigmaC1; 914 if (satData->system() == 'C') { 915 sigP3 *= BDS_WEIGHT_FACTOR; 916 } 917 ll(iObs) = satData->P3 - cmpValue(satData, false); 918 PP(iObs,iObs) = 1.0 / (sigP3 * sigP3) / (ellWgtCoef * ellWgtCoef); 919 for (int iPar = 1; iPar <= _params.size(); iPar++) { 920 AA(iObs, iPar) = _params[iPar-1]->partial(satData, false); 921 } 922 } 923 } 924 925 // 926 /////////////////////////////////////////////////////////////////////////// 927 QByteArray t_pppFilter::printRes(int iPhase, const ColumnVector& vv, 928 const QMap<QString, t_satData*>& satDataMap) { 929 930 Tracer tracer("t_pppFilter::printRes"); 931 932 ostringstream str; 933 str.setf(ios::fixed); 934 bool useObs; 935 QMapIterator<QString, t_satData*> it(satDataMap); 936 while (it.hasNext()) { 937 it.next(); 938 t_satData* satData = it.value(); 939 (iPhase == 0) ? useObs = OPT->codeLCs(satData->system()).size() : 940 useObs = OPT->ambLCs(satData->system()).size(); 941 if (satData->obsIndex != 0 && useObs) { 942 str << _time.timestr(1) 943 << " RES " << satData->prn.mid(0,3).toAscii().data() 944 << (iPhase ? " L3 " : " P3 ") 945 << setw(9) << setprecision(4) << vv(satData->obsIndex) << endl; 946 } 947 } 948 949 return QByteArray(str.str().c_str()); 950 } 951 952 // 953 /////////////////////////////////////////////////////////////////////////// 954 void t_pppFilter::findMaxRes(const ColumnVector& vv, 955 const QMap<QString, t_satData*>& satData, 956 QString& prnGPS, QString& prnGlo, 957 double& maxResGPS, double& maxResGlo) { 958 959 Tracer tracer("t_pppFilter::findMaxRes"); 960 961 maxResGPS = 0.0; 962 maxResGlo = 0.0; 963 964 QMapIterator<QString, t_satData*> it(satData); 965 while (it.hasNext()) { 966 it.next(); 967 t_satData* satData = it.value(); 968 if (satData->obsIndex != 0) { 969 QString prn = satData->prn; 970 if (prn[0] == 'R') { 971 if (fabs(vv(satData->obsIndex)) > maxResGlo) { 972 maxResGlo = fabs(vv(satData->obsIndex)); 973 prnGlo = prn; 974 } 975 } 976 else { 977 if (fabs(vv(satData->obsIndex)) > maxResGPS) { 978 maxResGPS = fabs(vv(satData->obsIndex)); 979 prnGPS = prn; 980 } 981 } 982 } 983 } 984 } 985 986 // Update Step (private - loop over outliers) 987 //////////////////////////////////////////////////////////////////////////// 988 t_irc t_pppFilter::update_p(t_epoData* epoData) { 989 990 Tracer tracer("t_pppFilter::update_p"); 991 992 // Save Variance-Covariance Matrix, and Status Vector 993 // -------------------------------------------------- 994 rememberState(epoData); 995 996 QString lastOutlierPrn; 997 998 // Try with all satellites, then with all minus one, etc. 999 // ------------------------------------------------------ 1000 while (selectSatellites(lastOutlierPrn, epoData->satData) == success) { 1001 1002 QByteArray strResCode; 1003 QByteArray strResPhase; 1004 1005 // Bancroft Solution 1006 // ----------------- 1007 if (cmpBancroft(epoData) != success) { 1008 break; 1009 } 1010 1011 // First update using code observations, then phase observations 1012 // ------------------------------------------------------------- 1013 bool usePhase = OPT->ambLCs('G').size() || OPT->ambLCs('R').size() || 1014 OPT->ambLCs('E').size() || OPT->ambLCs('C').size() ; 1015 1016 for (int iPhase = 0; iPhase <= (usePhase ? 1 : 0); iPhase++) { 1017 1018 // Status Prediction 1019 // ----------------- 1020 predict(iPhase, epoData); 1021 1022 // Create First-Design Matrix 1023 // -------------------------- 1024 unsigned nPar = _params.size(); 1025 unsigned nObs = 0; 1026 nObs = epoData->sizeAll(); 1027 bool useObs = false; 1028 char sys[] ={'G', 'R', 'E', 'C'}; 1029 for (unsigned ii = 0; ii < sizeof(sys); ii++) { 1030 const char s = sys[ii]; 1031 (iPhase == 0) ? useObs = OPT->codeLCs(s).size() : useObs = OPT->ambLCs(s).size(); 1032 if (!useObs) { 1033 nObs -= epoData->sizeSys(s); 1034 } 1035 } 1036 1037 // Prepare first-design Matrix, vector observed-computed 1038 // ----------------------------------------------------- 1039 Matrix AA(nObs, nPar); // first design matrix 1040 ColumnVector ll(nObs); // tems observed-computed 1041 DiagonalMatrix PP(nObs); PP = 0.0; 1042 1043 unsigned iObs = 0; 1044 QMapIterator<QString, t_satData*> it(epoData->satData); 1045 while (it.hasNext()) { 1046 it.next(); 1047 t_satData* satData = it.value(); 1048 QString prn = satData->prn; 1049 (iPhase == 0) ? useObs = OPT->codeLCs(satData->system()).size() : 1050 useObs = OPT->ambLCs(satData->system()).size(); 1051 if (useObs) { 1052 addObs(iPhase, iObs, satData, AA, ll, PP); 1053 } else { 1054 satData->obsIndex = 0; 1055 } 1056 } 1057 1058 // Compute Filter Update 1059 // --------------------- 1060 ColumnVector dx(nPar); dx = 0.0; 1061 kalman(AA, ll, PP, _QQ, dx); 1062 ColumnVector vv = ll - AA * dx; 1063 1064 // Print Residuals 1065 // --------------- 1066 if (iPhase == 0) { 1067 strResCode = printRes(iPhase, vv, epoData->satData); 1068 } 1069 else { 1070 strResPhase = printRes(iPhase, vv, epoData->satData); 1071 } 1072 1073 // Check the residuals 1074 // ------------------- 1075 lastOutlierPrn = outlierDetection(iPhase, vv, epoData->satData); 1076 1077 // No Outlier Detected 1078 // ------------------- 1079 if (lastOutlierPrn.isEmpty()) { 1080 1081 QVectorIterator<t_pppParam*> itPar(_params); 1082 while (itPar.hasNext()) { 1083 t_pppParam* par = itPar.next(); 1084 par->xx += dx(par->index); 1085 } 1086 1087 if (!usePhase || iPhase == 1) { 1088 if (_outlierGPS.size() > 0 || _outlierGlo.size() > 0) { 1089 LOG << "Neglected PRNs: "; 1090 if (!_outlierGPS.isEmpty()) { 1091 LOG << _outlierGPS.last().mid(0,3).toAscii().data() << ' '; 1092 } 1093 QStringListIterator itGlo(_outlierGlo); 1094 while (itGlo.hasNext()) { 1095 QString prn = itGlo.next(); 1096 LOG << prn.mid(0,3).toAscii().data() << ' '; 1097 } 180 1098 } 181 ll[iObs] = obs->obsValue(tLC) - obs->cmpValue(tLC) - DotProduct(_x0, AA.Row(iObs+1)); 182 PP[iObs] = 1.0 / (obs->sigma(tLC) * obs->sigma(tLC)); 1099 LOG << strResCode.data() << strResPhase.data(); 1100 1101 return success; 183 1102 } 184 1103 } 185 } 186 187 // Check number of observations, truncate matrices 188 // ----------------------------------------------- 189 if (iObs == -1) { 190 return failure; 191 } 192 AA = AA.Rows(1, iObs+1); 193 ll = ll.Rows(1, iObs+1); 194 PP = PP.SymSubMatrix(1, iObs+1); 195 196 // Kalman update step 197 // ------------------ 198 kalman(AA, ll, PP, _QFlt, _xFlt); 199 200 // Check Residuals 201 // --------------- 202 ColumnVector vv = AA * _xFlt - ll; 203 double maxOutlier = 0.0; 204 int maxOutlierIndex = -1; 205 t_lc::type maxOutlierLC = t_lc::dummy; 206 for (unsigned ii = 0; ii < usedObs.size(); ii++) { 207 const t_lc::type tLC = usedTypes[ii]; 208 double res = fabs(vv[ii]); 209 if (res > usedObs[ii]->maxRes(tLC)) { 210 if (res > fabs(maxOutlier)) { 211 maxOutlier = vv[ii]; 212 maxOutlierIndex = ii; 213 maxOutlierLC = tLC; 214 } 215 } 216 } 217 218 // Mark outlier or break outlier detection loop 219 // -------------------------------------------- 220 if (maxOutlierIndex > -1) { 221 t_pppSatObs* obs = usedObs[maxOutlierIndex]; 222 t_pppParam* par = 0; 223 LOG << epoTimeStr << " Outlier " << t_lc::toString(maxOutlierLC) << ' ' 224 << obs->prn().toString() << ' ' 225 << setw(8) << setprecision(4) << maxOutlier << endl; 226 for (unsigned iPar = 0; iPar < params.size(); iPar++) { 227 t_pppParam* hlp = params[iPar]; 228 if (hlp->type() == t_pppParam::amb && hlp->prn() == obs->prn() && 229 hlp->tLC() == usedTypes[maxOutlierIndex]) { 230 par = hlp; 231 } 232 } 233 if (par) { 234 if (par->ambResetCandidate()) { 235 resetAmb(par->prn(), obsVector, &QSav, &xSav); 236 } 237 else { 238 par->setAmbResetCandidate(); 239 obs->setOutlier(); 240 } 241 } 1104 1105 // Outlier Found 1106 // ------------- 242 1107 else { 243 obs->setOutlier(); 244 } 245 } 246 247 // Print Residuals 248 // --------------- 1108 restoreState(epoData); 1109 break; 1110 } 1111 1112 } // for iPhase 1113 1114 } // while selectSatellites 1115 1116 restoreState(epoData); 1117 return failure; 1118 } 1119 1120 // Remeber Original State Vector and Variance-Covariance Matrix 1121 //////////////////////////////////////////////////////////////////////////// 1122 void t_pppFilter::rememberState(t_epoData* epoData) { 1123 1124 _QQ_sav = _QQ; 1125 1126 QVectorIterator<t_pppParam*> itSav(_params_sav); 1127 while (itSav.hasNext()) { 1128 t_pppParam* par = itSav.next(); 1129 delete par; 1130 } 1131 _params_sav.clear(); 1132 1133 QVectorIterator<t_pppParam*> it(_params); 1134 while (it.hasNext()) { 1135 t_pppParam* par = it.next(); 1136 _params_sav.push_back(new t_pppParam(*par)); 1137 } 1138 1139 _epoData_sav->deepCopy(epoData); 1140 } 1141 1142 // Restore Original State Vector and Variance-Covariance Matrix 1143 //////////////////////////////////////////////////////////////////////////// 1144 void t_pppFilter::restoreState(t_epoData* epoData) { 1145 1146 _QQ = _QQ_sav; 1147 1148 QVectorIterator<t_pppParam*> it(_params); 1149 while (it.hasNext()) { 1150 t_pppParam* par = it.next(); 1151 delete par; 1152 } 1153 _params.clear(); 1154 1155 QVectorIterator<t_pppParam*> itSav(_params_sav); 1156 while (itSav.hasNext()) { 1157 t_pppParam* par = itSav.next(); 1158 _params.push_back(new t_pppParam(*par)); 1159 } 1160 1161 epoData->deepCopy(_epoData_sav); 1162 } 1163 1164 // 1165 //////////////////////////////////////////////////////////////////////////// 1166 t_irc t_pppFilter::selectSatellites(const QString& lastOutlierPrn, 1167 QMap<QString, t_satData*>& satData) { 1168 1169 // First Call 1170 // ---------- 1171 if (lastOutlierPrn.isEmpty()) { 1172 _outlierGPS.clear(); 1173 _outlierGlo.clear(); 1174 return success; 1175 } 1176 1177 // Second and next trials 1178 // ---------------------- 1179 else { 1180 1181 if (lastOutlierPrn[0] == 'R') { 1182 _outlierGlo << lastOutlierPrn; 1183 } 1184 1185 // Remove all Glonass Outliers 1186 // --------------------------- 1187 QStringListIterator it(_outlierGlo); 1188 while (it.hasNext()) { 1189 QString prn = it.next(); 1190 if (satData.contains(prn)) { 1191 delete satData.take(prn); 1192 } 1193 } 1194 1195 if (lastOutlierPrn[0] == 'R') { 1196 _outlierGPS.clear(); 1197 return success; 1198 } 1199 1200 // GPS Outlier appeared for the first time - try to delete it 1201 // ---------------------------------------------------------- 1202 if (_outlierGPS.indexOf(lastOutlierPrn) == -1) { 1203 _outlierGPS << lastOutlierPrn; 1204 if (satData.contains(lastOutlierPrn)) { 1205 delete satData.take(lastOutlierPrn); 1206 } 1207 return success; 1208 } 1209 1210 } 1211 1212 return failure; 1213 } 1214 1215 // 1216 //////////////////////////////////////////////////////////////////////////// 1217 double lorentz(const ColumnVector& aa, const ColumnVector& bb) { 1218 return aa(1)*bb(1) + aa(2)*bb(2) + aa(3)*bb(3) - aa(4)*bb(4); 1219 } 1220 1221 // 1222 //////////////////////////////////////////////////////////////////////////// 1223 void t_pppFilter::bancroft(const Matrix& BBpass, ColumnVector& pos) { 1224 1225 if (pos.Nrows() != 4) { 1226 pos.ReSize(4); 1227 } 1228 pos = 0.0; 1229 1230 for (int iter = 1; iter <= 2; iter++) { 1231 Matrix BB = BBpass; 1232 int mm = BB.Nrows(); 1233 for (int ii = 1; ii <= mm; ii++) { 1234 double xx = BB(ii,1); 1235 double yy = BB(ii,2); 1236 double traveltime = 0.072; 1237 if (iter > 1) { 1238 double zz = BB(ii,3); 1239 double rho = sqrt( (xx-pos(1)) * (xx-pos(1)) + 1240 (yy-pos(2)) * (yy-pos(2)) + 1241 (zz-pos(3)) * (zz-pos(3)) ); 1242 traveltime = rho / t_CST::c; 1243 } 1244 double angle = traveltime * t_CST::omega; 1245 double cosa = cos(angle); 1246 double sina = sin(angle); 1247 BB(ii,1) = cosa * xx + sina * yy; 1248 BB(ii,2) = -sina * xx + cosa * yy; 1249 } 1250 1251 Matrix BBB; 1252 if (mm > 4) { 1253 SymmetricMatrix hlp; hlp << BB.t() * BB; 1254 BBB = hlp.i() * BB.t(); 1255 } 249 1256 else { 250 for (unsigned jj = 0; jj < LCs.size(); jj++) { 251 for (unsigned ii = 0; ii < usedObs.size(); ii++) { 252 const t_lc::type tLC = usedTypes[ii]; 253 t_pppSatObs* obs = usedObs[ii]; 254 if (tLC == LCs[jj]) { 255 obs->setRes(tLC, vv[ii]); 256 LOG << epoTimeStr << " RES " 257 << left << setw(3) << t_lc::toString(tLC) << right << ' ' 258 << obs->prn().toString().substr(0,3) << ' ' 259 << setw(8) << setprecision(4) << vv[ii] << endl; 260 } 261 } 262 } 263 break; 264 } 265 } 266 267 return success; 268 } 269 270 // Cycle-Slip Detection 271 //////////////////////////////////////////////////////////////////////////// 272 t_irc t_pppFilter::detectCycleSlips(const vector<t_lc::type>& LCs, 273 const vector<t_pppSatObs*>& obsVector) { 274 275 const double SLIP = 20.0; // slip threshold 276 string epoTimeStr = string(_epoTime); 277 const vector<t_pppParam*>& params = _parlist->params(); 278 279 for (unsigned ii = 0; ii < LCs.size(); ii++) { 280 const t_lc::type& tLC = LCs[ii]; 281 if (t_lc::includesPhase(tLC)) { 282 for (unsigned iObs = 0; iObs < obsVector.size(); iObs++) { 283 const t_pppSatObs* obs = obsVector[iObs]; 284 285 // Check set Slips and Jump Counters 286 // --------------------------------- 287 bool slip = false; 288 289 if (obs->slip()) { 290 LOG << "cycle slip set (obs)" << endl;; 291 slip = true; 292 } 293 294 if (_slips[obs->prn()]._obsSlipCounter != -1 && 295 _slips[obs->prn()]._obsSlipCounter != obs->slipCounter()) { 296 LOG << "cycle slip set (obsSlipCounter)" << endl; 297 slip = true; 298 } 299 _slips[obs->prn()]._obsSlipCounter = obs->slipCounter(); 300 301 if (_slips[obs->prn()]._biasJumpCounter != -1 && 302 _slips[obs->prn()]._biasJumpCounter != obs->biasJumpCounter()) { 303 LOG << "cycle slip set (biasJumpCounter)" << endl; 304 slip = true; 305 } 306 _slips[obs->prn()]._biasJumpCounter = obs->biasJumpCounter(); 307 308 // Slip Set 309 // -------- 310 if (slip) { 311 resetAmb(obs->prn(), obsVector); 312 } 313 314 // Check Pre-Fit Residuals 315 // ----------------------- 316 else { 317 ColumnVector AA(params.size()); 318 for (unsigned iPar = 0; iPar < params.size(); iPar++) { 319 const t_pppParam* par = params[iPar]; 320 AA[iPar] = par->partial(_epoTime, obs, tLC); 321 } 322 323 double ll = obs->obsValue(tLC) - obs->cmpValue(tLC) - DotProduct(_x0, AA); 324 double vv = DotProduct(AA, _xFlt) - ll; 325 326 if (fabs(vv) > SLIP) { 327 LOG << epoTimeStr << " cycle slip detected " << t_lc::toString(tLC) << ' ' 328 << obs->prn().toString() << ' ' << setw(8) << setprecision(4) << vv << endl; 329 resetAmb(obs->prn(), obsVector); 330 } 331 } 332 } 333 } 334 } 335 336 return success; 337 } 338 339 // Reset Ambiguity Parameter (cycle slip) 340 //////////////////////////////////////////////////////////////////////////// 341 t_irc t_pppFilter::resetAmb(t_prn prn, const vector<t_pppSatObs*>& obsVector, 342 SymmetricMatrix* QSav, ColumnVector* xSav) { 343 t_irc irc = failure; 344 vector<t_pppParam*>& params = _parlist->params(); 345 for (unsigned iPar = 0; iPar < params.size(); iPar++) { 346 t_pppParam* par = params[iPar]; 347 if (par->type() == t_pppParam::amb && par->prn() == prn) { 348 int ind = par->indexNew(); 349 t_lc::type tLC = par->tLC(); 350 LOG << string(_epoTime) << " RESET " << par->toString() << endl; 351 delete par; par = new t_pppParam(t_pppParam::amb, prn, tLC, &obsVector); 352 par->setIndex(ind); 353 params[iPar] = par; 354 for (unsigned ii = 1; ii <= params.size(); ii++) { 355 _QFlt(ii, ind+1) = 0.0; 356 if (QSav) { 357 (*QSav)(ii, ind+1) = 0.0; 358 } 359 } 360 _QFlt(ind+1,ind+1) = par->sigma0() * par->sigma0(); 361 if (QSav) { 362 (*QSav)(ind+1,ind+1) = _QFlt(ind+1,ind+1); 363 } 364 _xFlt[ind] = 0.0; 365 if (xSav) { 366 (*xSav)[ind] = _xFlt[ind]; 367 } 368 _x0[ind] = par->x0(); 369 irc = success; 370 } 371 } 372 373 return irc; 374 } 375 376 // Compute various DOP Values 377 //////////////////////////////////////////////////////////////////////////// 378 void t_pppFilter::cmpDOP(const vector<t_pppSatObs*>& obsVector) { 379 380 _dop.reset(); 381 382 try { 383 const unsigned numPar = 4; 384 Matrix AA(obsVector.size(), numPar); 385 _numSat = 0; 386 for (unsigned ii = 0; ii < obsVector.size(); ii++) { 387 t_pppSatObs* obs = obsVector[ii]; 388 if (obs->isValid() && !obs->outlier()) { 389 ++_numSat; 390 for (unsigned iPar = 0; iPar < numPar; iPar++) { 391 const t_pppParam* par = _parlist->params()[iPar]; 392 AA[_numSat-1][iPar] = par->partial(_epoTime, obs, t_lc::c1); 393 } 394 } 395 } 396 if (_numSat < 4) { 397 return; 398 } 399 AA = AA.Rows(1, _numSat); 400 SymmetricMatrix NN; NN << AA.t() * AA; 401 SymmetricMatrix QQ = NN.i(); 402 403 _dop.P = sqrt(QQ(1,1) + QQ(2,2) + QQ(3,3)); 404 _dop.T = sqrt(QQ(4,4)); 405 _dop.G = sqrt(QQ(1,1) + QQ(2,2) + QQ(3,3) + QQ(4,4)); 406 } 407 catch (...) { 408 } 409 } 410 411 // Compute various DOP Values 412 //////////////////////////////////////////////////////////////////////////// 413 void t_pppFilter::predictCovCrdPart(const SymmetricMatrix& QFltOld) { 414 415 const vector<t_pppParam*>& params = _parlist->params(); 416 if (params.size() < 3) { 1257 BBB = BB.i(); 1258 } 1259 ColumnVector ee(mm); ee = 1.0; 1260 ColumnVector alpha(mm); alpha = 0.0; 1261 for (int ii = 1; ii <= mm; ii++) { 1262 alpha(ii) = lorentz(BB.Row(ii).t(),BB.Row(ii).t())/2.0; 1263 } 1264 ColumnVector BBBe = BBB * ee; 1265 ColumnVector BBBalpha = BBB * alpha; 1266 double aa = lorentz(BBBe, BBBe); 1267 double bb = lorentz(BBBe, BBBalpha)-1; 1268 double cc = lorentz(BBBalpha, BBBalpha); 1269 double root = sqrt(bb*bb-aa*cc); 1270 1271 Matrix hlpPos(4,2); 1272 hlpPos.Column(1) = (-bb-root)/aa * BBBe + BBBalpha; 1273 hlpPos.Column(2) = (-bb+root)/aa * BBBe + BBBalpha; 1274 1275 ColumnVector omc(2); 1276 for (int pp = 1; pp <= 2; pp++) { 1277 hlpPos(4,pp) = -hlpPos(4,pp); 1278 omc(pp) = BB(1,4) - 1279 sqrt( (BB(1,1)-hlpPos(1,pp)) * (BB(1,1)-hlpPos(1,pp)) + 1280 (BB(1,2)-hlpPos(2,pp)) * (BB(1,2)-hlpPos(2,pp)) + 1281 (BB(1,3)-hlpPos(3,pp)) * (BB(1,3)-hlpPos(3,pp)) ) - 1282 hlpPos(4,pp); 1283 } 1284 if ( fabs(omc(1)) > fabs(omc(2)) ) { 1285 pos = hlpPos.Column(2); 1286 } 1287 else { 1288 pos = hlpPos.Column(1); 1289 } 1290 } 1291 } 1292 1293 // 1294 //////////////////////////////////////////////////////////////////////////// 1295 void t_pppFilter::cmpDOP(t_epoData* epoData) { 1296 1297 Tracer tracer("t_pppFilter::cmpDOP"); 1298 1299 _numSat = 0; 1300 _pDop = 0.0; 1301 1302 if (_params.size() < 4) { 417 1303 return; 418 1304 } 419 1305 420 bool first = (params[0]->indexOld() < 0); 421 422 SymmetricMatrix Qneu(3); Qneu = 0.0; 423 for (unsigned ii = 0; ii < 3; ii++) { 424 const t_pppParam* par = params[ii]; 425 if (first) { 426 Qneu[ii][ii] = par->sigma0() * par->sigma0(); 427 } 428 else { 429 Qneu[ii][ii] = par->noise() * par->noise(); 430 } 431 } 432 433 const t_pppStation* sta = PPP_CLIENT->staRover(); 434 SymmetricMatrix Qxyz(3); 435 covariNEU_XYZ(Qneu, sta->ellApr().data(), Qxyz); 436 437 if (first) { 438 _QFlt.SymSubMatrix(1,3) = Qxyz; 439 } 440 else { 441 double dt = _epoTime - _firstEpoTime; 442 if (dt < OPT->_seedingTime) { 443 _QFlt.SymSubMatrix(1,3) = QFltOld.SymSubMatrix(1,3); 444 } 445 else { 446 _QFlt.SymSubMatrix(1,3) = QFltOld.SymSubMatrix(1,3) + Qxyz; 447 } 448 } 449 } 1306 const unsigned numPar = 4; 1307 Matrix AA(epoData->sizeAll(), numPar); 1308 QMapIterator<QString, t_satData*> it(epoData->satData); 1309 while (it.hasNext()) { 1310 it.next(); 1311 t_satData* satData = it.value(); 1312 _numSat += 1; 1313 for (unsigned iPar = 0; iPar < numPar; iPar++) { 1314 AA[_numSat-1][iPar] = _params[iPar]->partial(satData, false); 1315 } 1316 } 1317 if (_numSat < 4) { 1318 return; 1319 } 1320 AA = AA.Rows(1, _numSat); 1321 SymmetricMatrix NN; NN << AA.t() * AA; 1322 SymmetricMatrix QQ = NN.i(); 1323 1324 _pDop = sqrt(QQ(1,1) + QQ(2,2) + QQ(3,3)); 1325 } -
trunk/BNC/src/PPP/pppFilter.h
r6654 r7203 1 #ifndef FILTER_H 2 #define FILTER_H 3 4 #include <vector> 1 // Part of BNC, a utility for retrieving decoding and 2 // converting GNSS data streams from NTRIP broadcasters. 3 // 4 // Copyright (C) 2007 5 // German Federal Agency for Cartography and Geodesy (BKG) 6 // http://www.bkg.bund.de 7 // Czech Technical University Prague, Department of Geodesy 8 // http://www.fsv.cvut.cz 9 // 10 // Email: euref-ip@bkg.bund.de 11 // 12 // This program is free software; you can redistribute it and/or 13 // modify it under the terms of the GNU General Public License 14 // as published by the Free Software Foundation, version 2. 15 // 16 // This program is distributed in the hope that it will be useful, 17 // but WITHOUT ANY WARRANTY; without even the implied warranty of 18 // MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the 19 // GNU General Public License for more details. 20 // 21 // You should have received a copy of the GNU General Public License 22 // along with this program; if not, write to the Free Software 23 // Foundation, Inc., 59 Temple Place - Suite 330, Boston, MA 02111-1307, USA. 24 25 #ifndef PPPFILTER_H 26 #define PPPFILTER_H 27 28 #include <QtCore> 29 #include <QtNetwork> 5 30 #include <newmat.h> 6 #include "pppInclude.h" 7 #include " pppParlist.h"31 32 #include "bncconst.h" 8 33 #include "bnctime.h" 9 #include "t_prn.h" 34 35 class bncAntex; 10 36 11 37 namespace BNC_PPP { 12 38 13 class t_pppParlist; 14 class t_pppObsPool; 15 class t_pppSatObs; 39 class t_pppClient; 40 class t_pppOptions; 41 class t_epoData; 42 class t_satData; 43 class t_tides; 44 45 class t_satData { 46 public: 47 t_satData() { 48 obsIndex = 0; 49 P1 = 0.0; 50 P2 = 0.0; 51 P5 = 0.0; 52 P3 = 0.0; 53 L1 = 0.0; 54 L2 = 0.0; 55 L5 = 0.0; 56 L3 = 0.0; 57 lkA = 0.0; 58 lkB = 0.0; 59 } 60 ~t_satData() {} 61 bncTime tt; 62 QString prn; 63 double P1; 64 double P2; 65 double P5; 66 double P7; 67 double P3; 68 double L1; 69 double L2; 70 double L5; 71 double L7; 72 double L3; 73 ColumnVector xx; 74 ColumnVector vv; 75 double clk; 76 double eleSat; 77 double azSat; 78 double rho; 79 bool slipFlag; 80 double lambda3; 81 double lkA; 82 double lkB; 83 unsigned obsIndex; 84 char system() const {return prn.toAscii()[0];} 85 }; 86 87 class t_epoData { 88 public: 89 t_epoData() {} 90 91 ~t_epoData() { 92 clear(); 93 } 94 95 void clear() { 96 QMapIterator<QString, t_satData*> it(satData); 97 while (it.hasNext()) { 98 it.next(); 99 delete it.value(); 100 } 101 satData.clear(); 102 tt.reset(); 103 } 104 105 void deepCopy(const t_epoData* from) { 106 clear(); 107 tt = from->tt; 108 QMapIterator<QString, t_satData*> it(from->satData); 109 while (it.hasNext()) { 110 it.next(); 111 satData[it.key()] = new t_satData(*it.value()); 112 } 113 } 114 115 unsigned sizeSys(char system) const { 116 unsigned ans = 0; 117 QMapIterator<QString, t_satData*> it(satData); 118 while (it.hasNext()) { 119 it.next(); 120 if (it.value()->system() == system) { 121 ++ans; 122 } 123 } 124 return ans; 125 } 126 unsigned sizeAll() const {return satData.size();} 127 128 bncTime tt; 129 QMap<QString, t_satData*> satData; 130 }; 131 132 class t_pppParam { 133 public: 134 enum parType {CRD_X, CRD_Y, CRD_Z, RECCLK, TROPO, AMB_L3, 135 GLONASS_OFFSET, GALILEO_OFFSET, BDS_OFFSET}; 136 t_pppParam(parType typeIn, int indexIn, const QString& prn); 137 ~t_pppParam(); 138 double partial(t_satData* satData, bool phase); 139 bool isCrd() const { 140 return (type == CRD_X || type == CRD_Y || type == CRD_Z); 141 } 142 parType type; 143 double xx; 144 int index; 145 int index_old; 146 int numEpo; 147 QString prn; 148 }; 16 149 17 150 class t_pppFilter { 18 151 public: 19 t_pppFilter( );152 t_pppFilter(t_pppClient* pppClient); 20 153 ~t_pppFilter(); 21 22 t_irc processEpoch(t_pppObsPool* obsPool); 23 24 const ColumnVector& x() const {return _xFlt;} 25 const SymmetricMatrix& Q() const {return _QFlt;} 26 154 t_irc update(t_epoData* epoData); 155 bncTime time() const {return _time;} 156 const SymmetricMatrix& Q() const {return _QQ;} 157 const ColumnVector& neu() const {return _neu;} 27 158 int numSat() const {return _numSat;} 28 double PDOP() const {return _dop.P;} 29 double GDOP() const {return _dop.G;} 159 double PDOP() const {return _pDop;} 160 double x() const {return _params[0]->xx;} 161 double y() const {return _params[1]->xx;} 162 double z() const {return _params[2]->xx;} 163 double clk() const {return _params[3]->xx;} 164 double trp0() {return delay_saast(M_PI/2.0);} 30 165 double trp() const { 31 const std::vector<t_pppParam*>& par = _parlist->params();32 for (unsigned ii = 0; ii < par.size(); ++ii) {33 if (p ar[ii]->type() == t_pppParam::trp) {34 return x()[ii];35 } 36 } 37 return 0.0; 38 } ;166 for (int ii = 0; ii < _params.size(); ++ii) { 167 t_pppParam* pp = _params[ii]; 168 if (pp->type == t_pppParam::TROPO) { 169 return pp->xx; 170 } 171 } 172 return 0.0; 173 } 39 174 double trpStdev() const { 40 const std::vector<t_pppParam*>& par = _parlist->params();41 for (unsigned ii = 0; ii < par.size(); ++ii) {42 if (p ar[ii]->type() == t_pppParam::trp) {175 for (int ii = 0; ii < _params.size(); ++ii) { 176 t_pppParam* pp = _params[ii]; 177 if (pp->type == t_pppParam::TROPO) { 43 178 return sqrt(Q()[ii][ii]); 44 179 } 45 180 } 46 181 return 0.0; 47 }; 48 182 } 183 double Glonass_offset() const { 184 for (int ii = 0; ii < _params.size(); ++ii) { 185 t_pppParam* pp = _params[ii]; 186 if (pp->type == t_pppParam::GLONASS_OFFSET) { 187 return pp->xx; 188 } 189 } 190 return 0.0; 191 } 192 double Galileo_offset() const { 193 for (int ii = 0; ii < _params.size(); ++ii) { 194 t_pppParam* pp = _params[ii]; 195 if (pp->type == t_pppParam::GALILEO_OFFSET) { 196 return pp->xx; 197 } 198 } 199 return 0.0; 200 } 201 double Bds_offset() const { 202 for (int ii = 0; ii < _params.size(); ++ii) { 203 t_pppParam* pp = _params[ii]; 204 if (pp->type == t_pppParam::BDS_OFFSET) { 205 return pp->xx; 206 } 207 } 208 return 0.0; 209 } 49 210 private: 50 class t_slip { 51 public: 52 t_slip() { 53 _slip = false; 54 _obsSlipCounter = -1; 55 _biasJumpCounter = -1; 56 } 57 bool _slip; 58 int _obsSlipCounter; 59 int _biasJumpCounter; 60 }; 61 62 class t_dop { 63 public: 64 t_dop() {reset();} 65 void reset() {P = T = G = 0.0;} 66 double P; 67 double T; 68 double G; 69 }; 70 71 t_irc processSystem(const std::vector<t_lc::type>& LCs, 72 const std::vector<t_pppSatObs*>& obsVector); 73 74 t_irc detectCycleSlips(const std::vector<t_lc::type>& LCs, 75 const std::vector<t_pppSatObs*>& obsVector); 76 77 t_irc resetAmb(t_prn prn, const std::vector<t_pppSatObs*>& obsVector, 78 SymmetricMatrix* QSav = 0, ColumnVector* xSav = 0); 79 80 void cmpDOP(const std::vector<t_pppSatObs*>& obsVector); 81 82 void predictCovCrdPart(const SymmetricMatrix& QFltOld); 83 84 bncTime _epoTime; 85 t_pppParlist* _parlist; 86 SymmetricMatrix _QFlt; 87 ColumnVector _xFlt; 88 ColumnVector _x0; 89 t_slip _slips[t_prn::MAXPRN+1]; 90 int _numSat; 91 t_dop _dop; 92 bncTime _firstEpoTime; 211 void reset(); 212 t_irc cmpBancroft(t_epoData* epoData); 213 void cmpEle(t_satData* satData); 214 void addAmb(t_satData* satData); 215 void addObs(int iPhase, unsigned& iObs, t_satData* satData, 216 Matrix& AA, ColumnVector& ll, DiagonalMatrix& PP); 217 QByteArray printRes(int iPhase, const ColumnVector& vv, 218 const QMap<QString, t_satData*>& satDataMap); 219 void findMaxRes(const ColumnVector& vv, 220 const QMap<QString, t_satData*>& satData, 221 QString& prnGPS, QString& prnGlo, 222 double& maxResGPS, double& maxResGlo); 223 double cmpValue(t_satData* satData, bool phase); 224 double delay_saast(double Ele); 225 void predict(int iPhase, t_epoData* epoData); 226 t_irc update_p(t_epoData* epoData); 227 QString outlierDetection(int iPhase, const ColumnVector& vv, 228 QMap<QString, t_satData*>& satData); 229 230 double windUp(const QString& prn, const ColumnVector& rSat, 231 const ColumnVector& rRec); 232 233 bncTime _startTime; 234 235 void rememberState(t_epoData* epoData); 236 void restoreState(t_epoData* epoData); 237 238 t_irc selectSatellites(const QString& lastOutlierPrn, 239 QMap<QString, t_satData*>& satData); 240 241 void bancroft(const Matrix& BBpass, ColumnVector& pos); 242 243 void cmpDOP(t_epoData* epoData); 244 245 t_pppClient* _pppClient; 246 bncTime _time; 247 bncTime _lastTimeOK; 248 QVector<t_pppParam*> _params; 249 SymmetricMatrix _QQ; 250 QVector<t_pppParam*> _params_sav; 251 SymmetricMatrix _QQ_sav; 252 t_epoData* _epoData_sav; 253 ColumnVector _xcBanc; 254 ColumnVector _ellBanc; 255 QMap<QString, double> _windUpTime; 256 QMap<QString, double> _windUpSum; 257 QStringList _outlierGPS; 258 QStringList _outlierGlo; 259 bncAntex* _antex; 260 t_tides* _tides; 261 ColumnVector _neu; 262 int _numSat; 263 double _pDop; 93 264 }; 94 265 -
trunk/BNC/src/src.pri
r6875 r7203 117 117 } 118 118 119 exists(PPP) { 120 INCLUDEPATH += PPP 121 HEADERS += PPP/pppClient.h PPP/pppObsPool.h PPP/pppEphPool.h \ 122 PPP/pppStation.h PPP/pppFilter.h PPP/pppParlist.h \ 123 PPP/pppSatObs.h 124 SOURCES += PPP/pppClient.cpp PPP/pppObsPool.cpp PPP/pppEphPool.cpp \ 125 PPP/pppStation.cpp PPP/pppFilter.cpp PPP/pppParlist.cpp \ 126 PPP/pppSatObs.cpp 119 exists(PPP_AR) { 120 INCLUDEPATH += PPP_AR 121 DEFINES += USE_PPP_AR 122 HEADERS += PPP_AR/pppClient.h PPP_AR/pppObsPool.h PPP_AR/pppEphPool.h \ 123 PPP_AR/pppStation.h PPP_AR/pppFilter.h PPP_AR/pppParlist.h \ 124 PPP_AR/pppSatObs.h 125 SOURCES += PPP_AR/pppClient.cpp PPP_AR/pppObsPool.cpp PPP_AR/pppEphPool.cpp \ 126 PPP_AR/pppStation.cpp PPP_AR/pppFilter.cpp PPP_AR/pppParlist.cpp \ 127 PPP_AR/pppSatObs.cpp 127 128 } 128 129 else { 129 INCLUDEPATH += PPP _SSR_I130 DEFINES += USE_PPP _SSR_I131 HEADERS += PPP _SSR_I/pppClient.h PPP_SSR_I/pppFilter.h132 SOURCES += PPP _SSR_I/pppClient.cpp PPP_SSR_I/pppFilter.cpp130 INCLUDEPATH += PPP 131 DEFINES += USE_PPP 132 HEADERS += PPP/pppClient.h PPP/pppFilter.h 133 SOURCES += PPP/pppClient.cpp PPP/pppFilter.cpp 133 134 } 134 135
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