source: ntrip/trunk/BNC/src/PPP_free/bncmodel.cpp@ 6059

Last change on this file since 6059 was 6059, checked in by mervart, 10 years ago
File size: 36.4 KB
Line 
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/* -------------------------------------------------------------------------
26 * BKG NTRIP Client
27 * -------------------------------------------------------------------------
28 *
29 * Class: bncParam, bncModel
30 *
31 * Purpose: Model for PPP
32 *
33 * Author: L. Mervart
34 *
35 * Created: 01-Dec-2009
36 *
37 * Changes:
38 *
39 * -----------------------------------------------------------------------*/
40
41#include <iomanip>
42#include <cmath>
43#include <newmatio.h>
44#include <sstream>
45
46#include "bncmodel.h"
47#include "bncpppclient.h"
48#include "bnccore.h"
49#include "bncpppclient.h"
50#include "bancroft.h"
51#include "bncutils.h"
52#include "bncantex.h"
53#include "pppOptions.h"
54
55using namespace BNC_PPP;
56using namespace std;
57
58const unsigned MINOBS = 5;
59const double MINELE = 10.0 * M_PI / 180.0;
60const double MAXRES_CODE = 15.0;
61const double MAXRES_PHASE_GPS = 0.04;
62const double MAXRES_PHASE_GLONASS = 0.08;
63const double GLONASS_WEIGHT_FACTOR = 5.0;
64
65// Constructor
66////////////////////////////////////////////////////////////////////////////
67bncParam::bncParam(bncParam::parType typeIn, int indexIn,
68 const QString& prnIn) {
69 type = typeIn;
70 index = indexIn;
71 prn = prnIn;
72 index_old = 0;
73 xx = 0.0;
74 numEpo = 0;
75}
76
77// Destructor
78////////////////////////////////////////////////////////////////////////////
79bncParam::~bncParam() {
80}
81
82// Partial
83////////////////////////////////////////////////////////////////////////////
84double bncParam::partial(t_satData* satData, bool phase) {
85
86 Tracer tracer("bncParam::partial");
87
88 // Coordinates
89 // -----------
90 if (type == CRD_X) {
91 return (xx - satData->xx(1)) / satData->rho;
92 }
93 else if (type == CRD_Y) {
94 return (xx - satData->xx(2)) / satData->rho;
95 }
96 else if (type == CRD_Z) {
97 return (xx - satData->xx(3)) / satData->rho;
98 }
99
100 // Receiver Clocks
101 // ---------------
102 else if (type == RECCLK) {
103 return 1.0;
104 }
105
106 // Troposphere
107 // -----------
108 else if (type == TROPO) {
109 return 1.0 / sin(satData->eleSat);
110 }
111
112 // Glonass Offset
113 // --------------
114 else if (type == GLONASS_OFFSET) {
115 if (satData->prn[0] == 'R') {
116 return 1.0;
117 }
118 else {
119 return 0.0;
120 }
121 }
122
123 // Galileo Offset
124 // --------------
125 else if (type == GALILEO_OFFSET) {
126 if (satData->prn[0] == 'E') {
127 return 1.0;
128 }
129 else {
130 return 0.0;
131 }
132 }
133
134 // Ambiguities
135 // -----------
136 else if (type == AMB_L3) {
137 if (phase && satData->prn == prn) {
138 return 1.0;
139 }
140 else {
141 return 0.0;
142 }
143 }
144
145 // Default return
146 // --------------
147 return 0.0;
148}
149
150// Constructor
151////////////////////////////////////////////////////////////////////////////
152bncModel::bncModel(bncPPPclient* pppClient) {
153
154 _pppClient = pppClient;
155 _staID = pppClient->staID();
156 _opt = pppClient->opt();
157
158 // Antenna Name, ANTEX File
159 // ------------------------
160 _antex = 0;
161 if (!_opt->antexFile.isEmpty()) {
162 _antex = new bncAntex();
163 if (_antex->readFile(_opt->antexFile) != success) {
164 _pppClient->emitNewMessage("wrong ANTEX file", true);
165 delete _antex;
166 _antex = 0;
167 }
168 }
169
170 // Bancroft Coordinates
171 // --------------------
172 _xcBanc.ReSize(4); _xcBanc = 0.0;
173 _ellBanc.ReSize(3); _ellBanc = 0.0;
174
175 // Save copy of data (used in outlier detection)
176 // ---------------------------------------------
177 _epoData_sav = new t_epoData();
178}
179
180// Destructor
181////////////////////////////////////////////////////////////////////////////
182bncModel::~bncModel() {
183 for (int ii = 0; ii < _posAverage.size(); ++ii) {
184 delete _posAverage[ii];
185 }
186 delete _antex;
187 for (int iPar = 1; iPar <= _params.size(); iPar++) {
188 delete _params[iPar-1];
189 }
190 for (int iPar = 1; iPar <= _params_sav.size(); iPar++) {
191 delete _params_sav[iPar-1];
192 }
193 delete _epoData_sav;
194}
195
196// Reset Parameters and Variance-Covariance Matrix
197////////////////////////////////////////////////////////////////////////////
198void bncModel::reset() {
199
200 Tracer tracer("bncModel::reset");
201
202 double lastTrp = 0.0;
203 for (int ii = 0; ii < _params.size(); ii++) {
204 bncParam* pp = _params[ii];
205 if (pp->type == bncParam::TROPO) {
206 lastTrp = pp->xx;
207 }
208 delete pp;
209 }
210 _params.clear();
211
212 int nextPar = 0;
213 _params.push_back(new bncParam(bncParam::CRD_X, ++nextPar, ""));
214 _params.push_back(new bncParam(bncParam::CRD_Y, ++nextPar, ""));
215 _params.push_back(new bncParam(bncParam::CRD_Z, ++nextPar, ""));
216 _params.push_back(new bncParam(bncParam::RECCLK, ++nextPar, ""));
217 if (_opt->estTropo) {
218 _params.push_back(new bncParam(bncParam::TROPO, ++nextPar, ""));
219 }
220 if (_opt->useGlonass) {
221 _params.push_back(new bncParam(bncParam::GLONASS_OFFSET, ++nextPar, ""));
222 }
223 if (_opt->useGalileo) {
224 _params.push_back(new bncParam(bncParam::GALILEO_OFFSET, ++nextPar, ""));
225 }
226
227 _QQ.ReSize(_params.size());
228 _QQ = 0.0;
229 for (int iPar = 1; iPar <= _params.size(); iPar++) {
230 bncParam* pp = _params[iPar-1];
231 pp->xx = 0.0;
232 if (pp->isCrd()) {
233 _QQ(iPar,iPar) = _opt->sigCrd0 * _opt->sigCrd0;
234 }
235 else if (pp->type == bncParam::RECCLK) {
236 _QQ(iPar,iPar) = _opt->sigClk0 * _opt->sigClk0;
237 }
238 else if (pp->type == bncParam::TROPO) {
239 _QQ(iPar,iPar) = _opt->sigTrp0 * _opt->sigTrp0;
240 pp->xx = lastTrp;
241 }
242 else if (pp->type == bncParam::GLONASS_OFFSET) {
243 _QQ(iPar,iPar) = _opt->sigGlonassOffset0 * _opt->sigGlonassOffset0;
244 }
245 else if (pp->type == bncParam::GALILEO_OFFSET) {
246 _QQ(iPar,iPar) = _opt->sigGalileoOffset0 * _opt->sigGalileoOffset0;
247 }
248 }
249}
250
251// Bancroft Solution
252////////////////////////////////////////////////////////////////////////////
253t_irc bncModel::cmpBancroft(t_epoData* epoData) {
254
255 Tracer tracer("bncModel::cmpBancroft");
256
257 if (epoData->sizeSys('G') < MINOBS) {
258 _log += "bncModel::cmpBancroft: not enough data\n";
259 return failure;
260 }
261
262 Matrix BB(epoData->sizeSys('G'), 4);
263
264 QMapIterator<QString, t_satData*> it(epoData->satData);
265 int iObsBanc = 0;
266 while (it.hasNext()) {
267 it.next();
268 t_satData* satData = it.value();
269 if (satData->system() == 'G') {
270 ++iObsBanc;
271 QString prn = it.key();
272 BB(iObsBanc, 1) = satData->xx(1);
273 BB(iObsBanc, 2) = satData->xx(2);
274 BB(iObsBanc, 3) = satData->xx(3);
275 BB(iObsBanc, 4) = satData->P3 + satData->clk;
276 }
277 }
278
279 bancroft(BB, _xcBanc);
280
281 // Ellipsoidal Coordinates
282 // ------------------------
283 xyz2ell(_xcBanc.data(), _ellBanc.data());
284
285 // Compute Satellite Elevations
286 // ----------------------------
287 QMutableMapIterator<QString, t_satData*> im(epoData->satData);
288 while (im.hasNext()) {
289 im.next();
290 t_satData* satData = im.value();
291 cmpEle(satData);
292 if (satData->eleSat < MINELE) {
293 delete satData;
294 im.remove();
295 }
296 }
297
298 return success;
299}
300
301// Computed Value
302////////////////////////////////////////////////////////////////////////////
303double bncModel::cmpValue(t_satData* satData, bool phase) {
304
305 Tracer tracer("bncModel::cmpValue");
306
307 ColumnVector xRec(3);
308 xRec(1) = x();
309 xRec(2) = y();
310 xRec(3) = z();
311
312 double rho0 = (satData->xx - xRec).norm_Frobenius();
313 double dPhi = t_CST::omega * rho0 / t_CST::c;
314
315 xRec(1) = x() * cos(dPhi) - y() * sin(dPhi);
316 xRec(2) = y() * cos(dPhi) + x() * sin(dPhi);
317 xRec(3) = z();
318
319 tides(_time, xRec);
320
321 satData->rho = (satData->xx - xRec).norm_Frobenius();
322
323 double tropDelay = delay_saast(satData->eleSat) +
324 trp() / sin(satData->eleSat);
325
326 double wind = 0.0;
327 if (phase) {
328 wind = windUp(satData->prn, satData->xx, xRec) * satData->lambda3;
329 }
330
331 double offset = 0.0;
332 if (satData->prn[0] == 'R') {
333 offset = Glonass_offset();
334 }
335 else if (satData->prn[0] == 'E') {
336 offset = Galileo_offset();
337 }
338
339 double phaseCenter = 0.0;
340 if (_antex) {
341 bool found;
342 phaseCenter = _antex->pco(_opt->antennaName, satData->eleSat, found);
343 if (!found) {
344 _pppClient->emitNewMessage("ANTEX: antenna >"
345 + _opt->antennaName.toAscii() + "< not found", true);
346 }
347 }
348
349 double antennaOffset = 0.0;
350 if (_opt->antEccSet()) {
351 double cosa = cos(satData->azSat);
352 double sina = sin(satData->azSat);
353 double cose = cos(satData->eleSat);
354 double sine = sin(satData->eleSat);
355 antennaOffset = -_opt->antEccNEU[0] * cosa*cose
356 -_opt->antEccNEU[1] * sina*cose
357 -_opt->antEccNEU[2] * sine;
358 }
359
360 return satData->rho + phaseCenter + antennaOffset + clk()
361 + offset - satData->clk + tropDelay + wind;
362}
363
364// Tropospheric Model (Saastamoinen)
365////////////////////////////////////////////////////////////////////////////
366double bncModel::delay_saast(double Ele) {
367
368 Tracer tracer("bncModel::delay_saast");
369
370 double xyz[3];
371 xyz[0] = x();
372 xyz[1] = y();
373 xyz[2] = z();
374 double ell[3];
375 xyz2ell(xyz, ell);
376 double height = ell[2];
377
378 double pp = 1013.25 * pow(1.0 - 2.26e-5 * height, 5.225);
379 double TT = 18.0 - height * 0.0065 + 273.15;
380 double hh = 50.0 * exp(-6.396e-4 * height);
381 double ee = hh / 100.0 * exp(-37.2465 + 0.213166*TT - 0.000256908*TT*TT);
382
383 double h_km = height / 1000.0;
384
385 if (h_km < 0.0) h_km = 0.0;
386 if (h_km > 5.0) h_km = 5.0;
387 int ii = int(h_km + 1);
388 double href = ii - 1;
389
390 double bCor[6];
391 bCor[0] = 1.156;
392 bCor[1] = 1.006;
393 bCor[2] = 0.874;
394 bCor[3] = 0.757;
395 bCor[4] = 0.654;
396 bCor[5] = 0.563;
397
398 double BB = bCor[ii-1] + (bCor[ii]-bCor[ii-1]) * (h_km - href);
399
400 double zen = M_PI/2.0 - Ele;
401
402 return (0.002277/cos(zen)) * (pp + ((1255.0/TT)+0.05)*ee - BB*(tan(zen)*tan(zen)));
403}
404
405// Prediction Step of the Filter
406////////////////////////////////////////////////////////////////////////////
407void bncModel::predict(int iPhase, t_epoData* epoData) {
408
409 Tracer tracer("bncModel::predict");
410
411 if (iPhase == 0) {
412
413 bool firstCrd = false;
414 if (!_lastTimeOK.valid() || (_opt->maxSolGap > 0 && _time - _lastTimeOK > _opt->maxSolGap)) {
415 firstCrd = true;
416 _startTime = epoData->tt;
417 reset();
418 }
419
420 // Use different white noise for Quick-Start mode
421 // ----------------------------------------------
422 double sigCrdP_used = _opt->sigCrdP;
423 if ( _opt->quickStart > 0.0 && _opt->quickStart > (epoData->tt - _startTime) ) {
424 sigCrdP_used = 0.0;
425 }
426
427 // Predict Parameter values, add white noise
428 // -----------------------------------------
429 for (int iPar = 1; iPar <= _params.size(); iPar++) {
430 bncParam* pp = _params[iPar-1];
431
432 // Coordinates
433 // -----------
434 if (pp->type == bncParam::CRD_X) {
435 if (firstCrd) {
436 if (_opt->refCrdSet()) {
437 pp->xx = _opt->refCrd[0];
438 }
439 else {
440 pp->xx = _xcBanc(1);
441 }
442 }
443 _QQ(iPar,iPar) += sigCrdP_used * sigCrdP_used;
444 }
445 else if (pp->type == bncParam::CRD_Y) {
446 if (firstCrd) {
447 if (_opt->refCrdSet()) {
448 pp->xx = _opt->refCrd[1];
449 }
450 else {
451 pp->xx = _xcBanc(2);
452 }
453 }
454 _QQ(iPar,iPar) += sigCrdP_used * sigCrdP_used;
455 }
456 else if (pp->type == bncParam::CRD_Z) {
457 if (firstCrd) {
458 if (_opt->refCrdSet()) {
459 pp->xx = _opt->refCrd[2];
460 }
461 else {
462 pp->xx = _xcBanc(3);
463 }
464 }
465 _QQ(iPar,iPar) += sigCrdP_used * sigCrdP_used;
466 }
467
468 // Receiver Clocks
469 // ---------------
470 else if (pp->type == bncParam::RECCLK) {
471 pp->xx = _xcBanc(4);
472 for (int jj = 1; jj <= _params.size(); jj++) {
473 _QQ(iPar, jj) = 0.0;
474 }
475 _QQ(iPar,iPar) = _opt->sigClk0 * _opt->sigClk0;
476 }
477
478 // Tropospheric Delay
479 // ------------------
480 else if (pp->type == bncParam::TROPO) {
481 _QQ(iPar,iPar) += _opt->sigTrpP * _opt->sigTrpP;
482 }
483
484 // Glonass Offset
485 // --------------
486 else if (pp->type == bncParam::GLONASS_OFFSET) {
487 bool epoSpec = true;
488 if (epoSpec) {
489 pp->xx = 0.0;
490 for (int jj = 1; jj <= _params.size(); jj++) {
491 _QQ(iPar, jj) = 0.0;
492 }
493 _QQ(iPar,iPar) = _opt->sigGlonassOffset0 * _opt->sigGlonassOffset0;
494 }
495 else {
496 _QQ(iPar,iPar) += _opt->sigGlonassOffsetP * _opt->sigGlonassOffsetP;
497 }
498 }
499
500 // Galileo Offset
501 // --------------
502 else if (pp->type == bncParam::GALILEO_OFFSET) {
503 _QQ(iPar,iPar) += _opt->sigGalileoOffsetP * _opt->sigGalileoOffsetP;
504 }
505 }
506 }
507
508 // Add New Ambiguities if necessary
509 // --------------------------------
510 if (_opt->usePhase) {
511
512 // Make a copy of QQ and xx, set parameter indices
513 // -----------------------------------------------
514 SymmetricMatrix QQ_old = _QQ;
515
516 for (int iPar = 1; iPar <= _params.size(); iPar++) {
517 _params[iPar-1]->index_old = _params[iPar-1]->index;
518 _params[iPar-1]->index = 0;
519 }
520
521 // Remove Ambiguity Parameters without observations
522 // ------------------------------------------------
523 int iPar = 0;
524 QMutableVectorIterator<bncParam*> im(_params);
525 while (im.hasNext()) {
526 bncParam* par = im.next();
527 bool removed = false;
528 if (par->type == bncParam::AMB_L3) {
529 if (epoData->satData.find(par->prn) == epoData->satData.end()) {
530 removed = true;
531 delete par;
532 im.remove();
533 }
534 }
535 if (! removed) {
536 ++iPar;
537 par->index = iPar;
538 }
539 }
540
541 // Add new ambiguity parameters
542 // ----------------------------
543 QMapIterator<QString, t_satData*> it(epoData->satData);
544 while (it.hasNext()) {
545 it.next();
546 t_satData* satData = it.value();
547 addAmb(satData);
548 }
549
550 int nPar = _params.size();
551 _QQ.ReSize(nPar); _QQ = 0.0;
552 for (int i1 = 1; i1 <= nPar; i1++) {
553 bncParam* p1 = _params[i1-1];
554 if (p1->index_old != 0) {
555 _QQ(p1->index, p1->index) = QQ_old(p1->index_old, p1->index_old);
556 for (int i2 = 1; i2 <= nPar; i2++) {
557 bncParam* p2 = _params[i2-1];
558 if (p2->index_old != 0) {
559 _QQ(p1->index, p2->index) = QQ_old(p1->index_old, p2->index_old);
560 }
561 }
562 }
563 }
564
565 for (int ii = 1; ii <= nPar; ii++) {
566 bncParam* par = _params[ii-1];
567 if (par->index_old == 0) {
568 _QQ(par->index, par->index) = _opt->sigAmb0 * _opt->sigAmb0;
569 }
570 par->index_old = par->index;
571 }
572 }
573}
574
575// Update Step of the Filter (currently just a single-epoch solution)
576////////////////////////////////////////////////////////////////////////////
577t_irc bncModel::update(t_epoData* epoData) {
578
579 Tracer tracer("bncModel::update");
580
581 _log.clear();
582
583 _time = epoData->tt; // current epoch time
584
585 if (_opt->pppMode) {
586 _log += "Precise Point Positioning of Epoch "
587 + QByteArray(_time.timestr(1).c_str()) +
588 "\n---------------------------------------------------------------\n";
589 }
590 else {
591 _log += "Single Point Positioning of Epoch "
592 + QByteArray(_time.timestr(1).c_str()) +
593 "\n--------------------------------------------------------------\n";
594 }
595
596 // Outlier Detection Loop
597 // ----------------------
598 if (update_p(epoData) != success) {
599 _pppClient->emitNewMessage(_log, false);
600 return failure;
601 }
602
603 // Remember the Epoch-specific Results for the computation of means
604 // ----------------------------------------------------------------
605 pppPos* newPos = new pppPos;
606 newPos->time = epoData->tt;
607
608 // Set Solution Vector
609 // -------------------
610 ostringstream strB;
611 strB.setf(ios::fixed);
612 QVectorIterator<bncParam*> itPar(_params);
613 while (itPar.hasNext()) {
614 bncParam* par = itPar.next();
615
616 if (par->type == bncParam::RECCLK) {
617 strB << "\n clk = " << setw(10) << setprecision(3) << par->xx
618 << " +- " << setw(6) << setprecision(3)
619 << sqrt(_QQ(par->index,par->index));
620 }
621 else if (par->type == bncParam::AMB_L3) {
622 ++par->numEpo;
623 strB << "\n amb " << par->prn.toAscii().data() << " = "
624 << setw(10) << setprecision(3) << par->xx
625 << " +- " << setw(6) << setprecision(3)
626 << sqrt(_QQ(par->index,par->index))
627 << " nEpo = " << par->numEpo;
628 }
629 else if (par->type == bncParam::TROPO) {
630 double aprTrp = delay_saast(M_PI/2.0);
631 strB << "\n trp = " << par->prn.toAscii().data()
632 << setw(7) << setprecision(3) << aprTrp << " "
633 << setw(6) << setprecision(3) << showpos << par->xx << noshowpos
634 << " +- " << setw(6) << setprecision(3)
635 << sqrt(_QQ(par->index,par->index));
636 newPos->xnt[6] = aprTrp + par->xx;
637 }
638 else if (par->type == bncParam::GLONASS_OFFSET) {
639 strB << "\n offGlo = " << setw(10) << setprecision(3) << par->xx
640 << " +- " << setw(6) << setprecision(3)
641 << sqrt(_QQ(par->index,par->index));
642 }
643 else if (par->type == bncParam::GALILEO_OFFSET) {
644 strB << "\n offGal = " << setw(10) << setprecision(3) << par->xx
645 << " +- " << setw(6) << setprecision(3)
646 << sqrt(_QQ(par->index,par->index));
647 }
648 }
649 strB << '\n';
650 _log += strB.str().c_str();
651 _pppClient->emitNewMessage(_log, false);
652
653 // Final Message (both log file and screen)
654 // ----------------------------------------
655 ostringstream strC;
656 strC.setf(ios::fixed);
657 strC << _staID.data() << " PPP "
658 << epoData->tt.timestr(1) << " " << epoData->sizeAll() << " "
659 << setw(14) << setprecision(3) << x() << " +- "
660 << setw(6) << setprecision(3) << sqrt(_QQ(1,1)) << " "
661 << setw(14) << setprecision(3) << y() << " +- "
662 << setw(6) << setprecision(3) << sqrt(_QQ(2,2)) << " "
663 << setw(14) << setprecision(3) << z() << " +- "
664 << setw(6) << setprecision(3) << sqrt(_QQ(3,3));
665
666 // NEU Output
667 // ----------
668 if (_opt->refCrdSet()) {
669 newPos->xnt[0] = x() - _opt->refCrd[0];
670 newPos->xnt[1] = y() - _opt->refCrd[1];
671 newPos->xnt[2] = z() - _opt->refCrd[2];
672
673 double ellRef[3];
674 xyz2ell(_opt->refCrd, ellRef);
675 xyz2neu(ellRef, newPos->xnt, &newPos->xnt[3]);
676
677 strC << " NEU "
678 << setw(8) << setprecision(3) << newPos->xnt[3] << " "
679 << setw(8) << setprecision(3) << newPos->xnt[4] << " "
680 << setw(8) << setprecision(3) << newPos->xnt[5] << endl;
681
682 }
683
684 _pppClient->emitNewMessage(QByteArray(strC.str().c_str()), true);
685
686 if (_opt->pppAverage == 0.0) {
687 delete newPos;
688 }
689 else {
690
691 _posAverage.push_back(newPos);
692
693 // Compute the Mean
694 // ----------------
695 ColumnVector mean(7); mean = 0.0;
696
697 QMutableVectorIterator<pppPos*> it(_posAverage);
698 while (it.hasNext()) {
699 pppPos* pp = it.next();
700 if ( (epoData->tt - pp->time) >= _opt->pppAverage ) {
701 delete pp;
702 it.remove();
703 }
704 else {
705 for (int ii = 0; ii < 7; ++ii) {
706 mean[ii] += pp->xnt[ii];
707 }
708 }
709 }
710
711 int nn = _posAverage.size();
712
713 if (nn > 0) {
714
715 mean /= nn;
716
717 // Compute the Deviation
718 // ---------------------
719 ColumnVector std(7); std = 0.0;
720 QVectorIterator<pppPos*> it2(_posAverage);
721 while (it2.hasNext()) {
722 pppPos* pp = it2.next();
723 for (int ii = 0; ii < 7; ++ii) {
724 std[ii] += (pp->xnt[ii] - mean[ii]) * (pp->xnt[ii] - mean[ii]);
725 }
726 }
727 for (int ii = 0; ii < 7; ++ii) {
728 std[ii] = sqrt(std[ii] / nn);
729 }
730
731 if (_opt->refCrdSet()) {
732 ostringstream strD; strD.setf(ios::fixed);
733 strD << _staID.data() << " AVE-XYZ "
734 << epoData->tt.timestr(1) << " "
735 << setw(13) << setprecision(3) << mean[0] + _opt->refCrd[0] << " +- "
736 << setw(6) << setprecision(3) << std[0] << " "
737 << setw(14) << setprecision(3) << mean[1] + _opt->refCrd[1] << " +- "
738 << setw(6) << setprecision(3) << std[1] << " "
739 << setw(14) << setprecision(3) << mean[2] + _opt->refCrd[2] << " +- "
740 << setw(6) << setprecision(3) << std[2];
741 _pppClient->emitNewMessage(QByteArray(strD.str().c_str()), true);
742
743 ostringstream strE; strE.setf(ios::fixed);
744 strE << _staID.data() << " AVE-NEU "
745 << epoData->tt.timestr(1) << " "
746 << setw(13) << setprecision(3) << mean[3] << " +- "
747 << setw(6) << setprecision(3) << std[3] << " "
748 << setw(14) << setprecision(3) << mean[4] << " +- "
749 << setw(6) << setprecision(3) << std[4] << " "
750 << setw(14) << setprecision(3) << mean[5] << " +- "
751 << setw(6) << setprecision(3) << std[5];
752 _pppClient->emitNewMessage(QByteArray(strE.str().c_str()), true);
753
754 if (_opt->estTropo) {
755 ostringstream strF; strF.setf(ios::fixed);
756 strF << _staID.data() << " AVE-TRP "
757 << epoData->tt.timestr(1) << " "
758 << setw(13) << setprecision(3) << mean[6] << " +- "
759 << setw(6) << setprecision(3) << std[6] << endl;
760 _pppClient->emitNewMessage(QByteArray(strF.str().c_str()), true);
761 }
762 }
763 }
764 }
765
766 _lastTimeOK = _time; // remember time of last successful update
767 return success;
768}
769
770// Outlier Detection
771////////////////////////////////////////////////////////////////////////////
772QString bncModel::outlierDetection(int iPhase, const ColumnVector& vv,
773 QMap<QString, t_satData*>& satData) {
774
775 Tracer tracer("bncModel::outlierDetection");
776
777 QString prnGPS;
778 QString prnGlo;
779 double maxResGPS = 0.0;
780 double maxResGlo = 0.0;
781 findMaxRes(vv, satData, prnGPS, prnGlo, maxResGPS, maxResGlo);
782
783 if (iPhase == 1) {
784 if (maxResGlo > MAXRES_PHASE_GLONASS) {
785 _log += "Outlier Phase " + prnGlo + " "
786 + QByteArray::number(maxResGlo, 'f', 3) + "\n";
787 return prnGlo;
788 }
789 else if (maxResGPS > MAXRES_PHASE_GPS) {
790 _log += "Outlier Phase " + prnGPS + " "
791 + QByteArray::number(maxResGPS, 'f', 3) + "\n";
792 return prnGPS;
793 }
794 }
795 else if (iPhase == 0 && maxResGPS > MAXRES_CODE) {
796 _log += "Outlier Code " + prnGPS + " "
797 + QByteArray::number(maxResGPS, 'f', 3) + "\n";
798 return prnGPS;
799 }
800
801 return QString();
802}
803
804//
805//////////////////////////////////////////////////////////////////////////////
806void bncModel::kalman(const Matrix& AA, const ColumnVector& ll,
807 const DiagonalMatrix& PP,
808 SymmetricMatrix& QQ, ColumnVector& dx) {
809
810 Tracer tracer("bncModel::kalman");
811
812 int nPar = AA.Ncols();
813 int nObs = AA.Nrows();
814 UpperTriangularMatrix SS = Cholesky(QQ).t();
815
816 Matrix SA = SS*AA.t();
817 Matrix SRF(nObs+nPar, nObs+nPar); SRF = 0;
818 for (int ii = 1; ii <= nObs; ++ii) {
819 SRF(ii,ii) = 1.0 / sqrt(PP(ii,ii));
820 }
821
822 SRF.SubMatrix (nObs+1, nObs+nPar, 1, nObs) = SA;
823 SRF.SymSubMatrix(nObs+1, nObs+nPar) = SS;
824
825 UpperTriangularMatrix UU;
826 QRZ(SRF, UU);
827
828 SS = UU.SymSubMatrix(nObs+1, nObs+nPar);
829 UpperTriangularMatrix SH_rt = UU.SymSubMatrix(1, nObs);
830 Matrix YY = UU.SubMatrix(1, nObs, nObs+1, nObs+nPar);
831
832 UpperTriangularMatrix SHi = SH_rt.i();
833
834 Matrix KT = SHi * YY;
835 SymmetricMatrix Hi; Hi << SHi * SHi.t();
836
837 dx = KT.t() * ll;
838 QQ << (SS.t() * SS);
839}
840
841// Phase Wind-Up Correction
842///////////////////////////////////////////////////////////////////////////
843double bncModel::windUp(const QString& prn, const ColumnVector& rSat,
844 const ColumnVector& rRec) {
845
846 Tracer tracer("bncModel::windUp");
847
848 double Mjd = _time.mjd() + _time.daysec() / 86400.0;
849
850 // First time - initialize to zero
851 // -------------------------------
852 if (!_windUpTime.contains(prn)) {
853 _windUpSum[prn] = 0.0;
854 }
855
856 // Compute the correction for new time
857 // -----------------------------------
858 if (!_windUpTime.contains(prn) || _windUpTime[prn] != Mjd) {
859 _windUpTime[prn] = Mjd;
860
861 // Unit Vector GPS Satellite --> Receiver
862 // --------------------------------------
863 ColumnVector rho = rRec - rSat;
864 rho /= rho.norm_Frobenius();
865
866 // GPS Satellite unit Vectors sz, sy, sx
867 // -------------------------------------
868 ColumnVector sz = -rSat / rSat.norm_Frobenius();
869
870 ColumnVector xSun = Sun(Mjd);
871 xSun /= xSun.norm_Frobenius();
872
873 ColumnVector sy = crossproduct(sz, xSun);
874 ColumnVector sx = crossproduct(sy, sz);
875
876 // Effective Dipole of the GPS Satellite Antenna
877 // ---------------------------------------------
878 ColumnVector dipSat = sx - rho * DotProduct(rho,sx)
879 - crossproduct(rho, sy);
880
881 // Receiver unit Vectors rx, ry
882 // ----------------------------
883 ColumnVector rx(3);
884 ColumnVector ry(3);
885
886 double recEll[3]; xyz2ell(rRec.data(), recEll) ;
887 double neu[3];
888
889 neu[0] = 1.0;
890 neu[1] = 0.0;
891 neu[2] = 0.0;
892 neu2xyz(recEll, neu, rx.data());
893
894 neu[0] = 0.0;
895 neu[1] = -1.0;
896 neu[2] = 0.0;
897 neu2xyz(recEll, neu, ry.data());
898
899 // Effective Dipole of the Receiver Antenna
900 // ----------------------------------------
901 ColumnVector dipRec = rx - rho * DotProduct(rho,rx)
902 + crossproduct(rho, ry);
903
904 // Resulting Effect
905 // ----------------
906 double alpha = DotProduct(dipSat,dipRec) /
907 (dipSat.norm_Frobenius() * dipRec.norm_Frobenius());
908
909 if (alpha > 1.0) alpha = 1.0;
910 if (alpha < -1.0) alpha = -1.0;
911
912 double dphi = acos(alpha) / 2.0 / M_PI; // in cycles
913
914 if ( DotProduct(rho, crossproduct(dipSat, dipRec)) < 0.0 ) {
915 dphi = -dphi;
916 }
917
918 _windUpSum[prn] = floor(_windUpSum[prn] - dphi + 0.5) + dphi;
919 }
920
921 return _windUpSum[prn];
922}
923
924//
925///////////////////////////////////////////////////////////////////////////
926void bncModel::cmpEle(t_satData* satData) {
927 Tracer tracer("bncModel::cmpEle");
928 ColumnVector rr = satData->xx - _xcBanc.Rows(1,3);
929 double rho = rr.norm_Frobenius();
930
931 double neu[3];
932 xyz2neu(_ellBanc.data(), rr.data(), neu);
933
934 satData->eleSat = acos( sqrt(neu[0]*neu[0] + neu[1]*neu[1]) / rho );
935 if (neu[2] < 0) {
936 satData->eleSat *= -1.0;
937 }
938 satData->azSat = atan2(neu[1], neu[0]);
939}
940
941//
942///////////////////////////////////////////////////////////////////////////
943void bncModel::addAmb(t_satData* satData) {
944 Tracer tracer("bncModel::addAmb");
945 bool found = false;
946 for (int iPar = 1; iPar <= _params.size(); iPar++) {
947 if (_params[iPar-1]->type == bncParam::AMB_L3 &&
948 _params[iPar-1]->prn == satData->prn) {
949 found = true;
950 break;
951 }
952 }
953 if (!found) {
954 bncParam* par = new bncParam(bncParam::AMB_L3,
955 _params.size()+1, satData->prn);
956 _params.push_back(par);
957 par->xx = satData->L3 - cmpValue(satData, true);
958 }
959}
960
961//
962///////////////////////////////////////////////////////////////////////////
963void bncModel::addObs(int iPhase, unsigned& iObs, t_satData* satData,
964 Matrix& AA, ColumnVector& ll, DiagonalMatrix& PP) {
965
966 Tracer tracer("bncModel::addObs");
967
968 const double ELEWGHT = 20.0;
969 double ellWgtCoef = 1.0;
970 double eleD = satData->eleSat * 180.0 / M_PI;
971 if (eleD < ELEWGHT) {
972 ellWgtCoef = 1.5 - 0.5 / (ELEWGHT - 10.0) * (eleD - 10.0);
973 }
974
975 // Remember Observation Index
976 // --------------------------
977 ++iObs;
978 satData->obsIndex = iObs;
979
980 // Phase Observations
981 // ------------------
982 if (iPhase == 1) {
983 ll(iObs) = satData->L3 - cmpValue(satData, true);
984 double sigL3 = _opt->sigL3;
985 if (satData->system() == 'R') {
986 sigL3 *= GLONASS_WEIGHT_FACTOR;
987 }
988 PP(iObs,iObs) = 1.0 / (sigL3 * sigL3) / (ellWgtCoef * ellWgtCoef);
989 for (int iPar = 1; iPar <= _params.size(); iPar++) {
990 if (_params[iPar-1]->type == bncParam::AMB_L3 &&
991 _params[iPar-1]->prn == satData->prn) {
992 ll(iObs) -= _params[iPar-1]->xx;
993 }
994 AA(iObs, iPar) = _params[iPar-1]->partial(satData, true);
995 }
996 }
997
998 // Code Observations
999 // -----------------
1000 else {
1001 ll(iObs) = satData->P3 - cmpValue(satData, false);
1002 PP(iObs,iObs) = 1.0 / (_opt->sigP3 * _opt->sigP3) / (ellWgtCoef * ellWgtCoef);
1003 for (int iPar = 1; iPar <= _params.size(); iPar++) {
1004 AA(iObs, iPar) = _params[iPar-1]->partial(satData, false);
1005 }
1006 }
1007}
1008
1009//
1010///////////////////////////////////////////////////////////////////////////
1011QByteArray bncModel::printRes(int iPhase, const ColumnVector& vv,
1012 const QMap<QString, t_satData*>& satDataMap) {
1013
1014 Tracer tracer("bncModel::printRes");
1015
1016 ostringstream str;
1017 str.setf(ios::fixed);
1018
1019 QMapIterator<QString, t_satData*> it(satDataMap);
1020 while (it.hasNext()) {
1021 it.next();
1022 t_satData* satData = it.value();
1023 if (satData->obsIndex != 0) {
1024 str << _time.timestr(1)
1025 << " RES " << satData->prn.toAscii().data()
1026 << (iPhase ? " L3 " : " P3 ")
1027 << setw(9) << setprecision(4) << vv(satData->obsIndex) << endl;
1028 }
1029 }
1030
1031 return QByteArray(str.str().c_str());
1032}
1033
1034//
1035///////////////////////////////////////////////////////////////////////////
1036void bncModel::findMaxRes(const ColumnVector& vv,
1037 const QMap<QString, t_satData*>& satData,
1038 QString& prnGPS, QString& prnGlo,
1039 double& maxResGPS, double& maxResGlo) {
1040
1041 Tracer tracer("bncModel::findMaxRes");
1042
1043 maxResGPS = 0.0;
1044 maxResGlo = 0.0;
1045
1046 QMapIterator<QString, t_satData*> it(satData);
1047 while (it.hasNext()) {
1048 it.next();
1049 t_satData* satData = it.value();
1050 if (satData->obsIndex != 0) {
1051 QString prn = satData->prn;
1052 if (prn[0] == 'R') {
1053 if (fabs(vv(satData->obsIndex)) > maxResGlo) {
1054 maxResGlo = fabs(vv(satData->obsIndex));
1055 prnGlo = prn;
1056 }
1057 }
1058 else {
1059 if (fabs(vv(satData->obsIndex)) > maxResGPS) {
1060 maxResGPS = fabs(vv(satData->obsIndex));
1061 prnGPS = prn;
1062 }
1063 }
1064 }
1065 }
1066}
1067
1068// Update Step (private - loop over outliers)
1069////////////////////////////////////////////////////////////////////////////
1070t_irc bncModel::update_p(t_epoData* epoData) {
1071
1072 Tracer tracer("bncModel::update_p");
1073
1074 // Save Variance-Covariance Matrix, and Status Vector
1075 // --------------------------------------------------
1076 rememberState(epoData);
1077
1078 QString lastOutlierPrn;
1079
1080 // Try with all satellites, then with all minus one, etc.
1081 // ------------------------------------------------------
1082 while (selectSatellites(lastOutlierPrn, epoData->satData) == success) {
1083
1084 QByteArray strResCode;
1085 QByteArray strResPhase;
1086
1087 // Bancroft Solution
1088 // -----------------
1089 if (cmpBancroft(epoData) != success) {
1090 break;
1091 }
1092
1093 // First update using code observations, then phase observations
1094 // -------------------------------------------------------------
1095 for (int iPhase = 0; iPhase <= (_opt->usePhase ? 1 : 0); iPhase++) {
1096
1097 // Status Prediction
1098 // -----------------
1099 predict(iPhase, epoData);
1100
1101 // Create First-Design Matrix
1102 // --------------------------
1103 unsigned nPar = _params.size();
1104 unsigned nObs = 0;
1105 if (iPhase == 0) {
1106 nObs = epoData->sizeAll() - epoData->sizeSys('R'); // Glonass code not used
1107 }
1108 else {
1109 nObs = epoData->sizeAll();
1110 }
1111
1112 // Prepare first-design Matrix, vector observed-computed
1113 // -----------------------------------------------------
1114 Matrix AA(nObs, nPar); // first design matrix
1115 ColumnVector ll(nObs); // tems observed-computed
1116 DiagonalMatrix PP(nObs); PP = 0.0;
1117
1118 unsigned iObs = 0;
1119 QMapIterator<QString, t_satData*> it(epoData->satData);
1120 while (it.hasNext()) {
1121 it.next();
1122 t_satData* satData = it.value();
1123 if (iPhase == 1 || satData->system() != 'R') {
1124 QString prn = satData->prn;
1125 addObs(iPhase, iObs, satData, AA, ll, PP);
1126 }
1127 }
1128
1129 // Compute Filter Update
1130 // ---------------------
1131 ColumnVector dx;
1132 kalman(AA, ll, PP, _QQ, dx);
1133 ColumnVector vv = ll - AA * dx;
1134
1135 // Print Residuals
1136 // ---------------
1137 if (iPhase == 0) {
1138 strResCode = printRes(iPhase, vv, epoData->satData);
1139 }
1140 else {
1141 strResPhase = printRes(iPhase, vv, epoData->satData);
1142 }
1143
1144 // Check the residuals
1145 // -------------------
1146 lastOutlierPrn = outlierDetection(iPhase, vv, epoData->satData);
1147
1148 // No Outlier Detected
1149 // -------------------
1150 if (lastOutlierPrn.isEmpty()) {
1151
1152 QVectorIterator<bncParam*> itPar(_params);
1153 while (itPar.hasNext()) {
1154 bncParam* par = itPar.next();
1155 par->xx += dx(par->index);
1156 }
1157
1158 if (!_opt->usePhase || iPhase == 1) {
1159 if (_outlierGPS.size() > 0 || _outlierGlo.size() > 0) {
1160 _log += "Neglected PRNs: ";
1161 if (!_outlierGPS.isEmpty()) {
1162 _log += _outlierGPS.last() + ' ';
1163 }
1164 QStringListIterator itGlo(_outlierGlo);
1165 while (itGlo.hasNext()) {
1166 QString prn = itGlo.next();
1167 _log += prn + ' ';
1168 }
1169 }
1170 _log += '\n';
1171
1172 _log += strResCode + strResPhase;
1173
1174 return success;
1175 }
1176 }
1177
1178 // Outlier Found
1179 // -------------
1180 else {
1181 restoreState(epoData);
1182 break;
1183 }
1184
1185 } // for iPhase
1186
1187 } // while selectSatellites
1188
1189 restoreState(epoData);
1190 return failure;
1191}
1192
1193// Remeber Original State Vector and Variance-Covariance Matrix
1194////////////////////////////////////////////////////////////////////////////
1195void bncModel::rememberState(t_epoData* epoData) {
1196
1197 _QQ_sav = _QQ;
1198
1199 QVectorIterator<bncParam*> itSav(_params_sav);
1200 while (itSav.hasNext()) {
1201 bncParam* par = itSav.next();
1202 delete par;
1203 }
1204 _params_sav.clear();
1205
1206 QVectorIterator<bncParam*> it(_params);
1207 while (it.hasNext()) {
1208 bncParam* par = it.next();
1209 _params_sav.push_back(new bncParam(*par));
1210 }
1211
1212 _epoData_sav->deepCopy(epoData);
1213}
1214
1215// Restore Original State Vector and Variance-Covariance Matrix
1216////////////////////////////////////////////////////////////////////////////
1217void bncModel::restoreState(t_epoData* epoData) {
1218
1219 _QQ = _QQ_sav;
1220
1221 QVectorIterator<bncParam*> it(_params);
1222 while (it.hasNext()) {
1223 bncParam* par = it.next();
1224 delete par;
1225 }
1226 _params.clear();
1227
1228 QVectorIterator<bncParam*> itSav(_params_sav);
1229 while (itSav.hasNext()) {
1230 bncParam* par = itSav.next();
1231 _params.push_back(new bncParam(*par));
1232 }
1233
1234 epoData->deepCopy(_epoData_sav);
1235}
1236
1237//
1238////////////////////////////////////////////////////////////////////////////
1239t_irc bncModel::selectSatellites(const QString& lastOutlierPrn,
1240 QMap<QString, t_satData*>& satData) {
1241
1242 // First Call
1243 // ----------
1244 if (lastOutlierPrn.isEmpty()) {
1245 _outlierGPS.clear();
1246 _outlierGlo.clear();
1247 return success;
1248 }
1249
1250 // Second and next trials
1251 // ----------------------
1252 else {
1253
1254 if (lastOutlierPrn[0] == 'R') {
1255 _outlierGlo << lastOutlierPrn;
1256 }
1257
1258 // Remove all Glonass Outliers
1259 // ---------------------------
1260 QStringListIterator it(_outlierGlo);
1261 while (it.hasNext()) {
1262 QString prn = it.next();
1263 if (satData.contains(prn)) {
1264 delete satData.take(prn);
1265 }
1266 }
1267
1268 if (lastOutlierPrn[0] == 'R') {
1269 _outlierGPS.clear();
1270 return success;
1271 }
1272
1273 // GPS Outlier appeared for the first time - try to delete it
1274 // ----------------------------------------------------------
1275 if (_outlierGPS.indexOf(lastOutlierPrn) == -1) {
1276 _outlierGPS << lastOutlierPrn;
1277 if (satData.contains(lastOutlierPrn)) {
1278 delete satData.take(lastOutlierPrn);
1279 }
1280 return success;
1281 }
1282
1283 }
1284
1285 return failure;
1286}
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