source: ntrip/trunk/BNC/src/upload/bncrtnetuploadcaster.cpp@ 9188

Last change on this file since 9188 was 9179, checked in by stuerze, 4 years ago

check if orbit and clock corrections are in defined ranges is added

File size: 38.5 KB
Line 
1/* -------------------------------------------------------------------------
2 * BKG NTRIP Server
3 * -------------------------------------------------------------------------
4 *
5 * Class: bncRtnetUploadCaster
6 *
7 * Purpose: Connection to NTRIP Caster
8 *
9 * Author: L. Mervart
10 *
11 * Created: 29-Mar-2011
12 *
13 * Changes:
14 *
15 * -----------------------------------------------------------------------*/
16
17#include <math.h>
18#include "bncrtnetuploadcaster.h"
19#include "bncsettings.h"
20#include "bncephuser.h"
21#include "bncclockrinex.h"
22#include "bncsp3.h"
23#include "gnss.h"
24
25using namespace std;
26
27// Constructor
28////////////////////////////////////////////////////////////////////////////
29bncRtnetUploadCaster::bncRtnetUploadCaster(const QString& mountpoint,
30 const QString& outHost, int outPort,
31 const QString& ntripVersion,
32 const QString& userName, const QString& password,
33 const QString& crdTrafo, const QString& ssrFormat, bool CoM, const QString& sp3FileName,
34 const QString& rnxFileName, int PID, int SID, int IOD, int iRow) :
35 bncUploadCaster(mountpoint, outHost, outPort, ntripVersion, userName, password, iRow, 0) {
36
37 if (!mountpoint.isEmpty()) {
38 _casterID += mountpoint;
39 }
40 if (!outHost.isEmpty()) {
41 _casterID += " " + outHost;
42 if (outPort) {
43 _casterID += ":" + QString("%1").arg(outPort, 10);
44 }
45 }
46 if (!crdTrafo.isEmpty()) {
47 _casterID += " " + crdTrafo;
48 }
49 if (!sp3FileName.isEmpty()) {
50 _casterID += " " + sp3FileName;
51 }
52 if (!rnxFileName.isEmpty()) {
53 _casterID += " " + rnxFileName;
54 }
55
56 _crdTrafo = crdTrafo;
57
58 _ssrFormat = ssrFormat;
59
60 _ssrCorr = 0;
61 if (_ssrFormat == "IGS-SSR") {
62 _ssrCorr = new SsrCorrIgs();
63 }
64 else if (_ssrFormat == "RTCM-SSR") {
65 _ssrCorr = new SsrCorrRtcm();
66 }
67
68 _CoM = CoM;
69 _PID = PID;
70 _SID = SID;
71 _IOD = IOD;
72
73 // Member that receives the ephemeris
74 // ----------------------------------
75 _ephUser = new bncEphUser(true);
76
77 bncSettings settings;
78 QString intr = settings.value("uploadIntr").toString();
79 QStringList hlp = settings.value("cmbStreams").toStringList();
80 _samplRtcmEphCorr = settings.value("uploadSamplRtcmEphCorr").toDouble();
81 if (hlp.size() > 1) { // combination stream upload
82 _samplRtcmClkCorr = settings.value("cmbSampl").toInt();
83 }
84 else { // single stream upload or sp3 file generation
85 _samplRtcmClkCorr = 5; // default
86 }
87 int samplClkRnx = settings.value("uploadSamplClkRnx").toInt();
88 int samplSp3 = settings.value("uploadSamplSp3").toInt() * 60;
89
90 if (_samplRtcmEphCorr == 0.0) {
91 _usedEph = 0;
92 }
93 else {
94 _usedEph = new QMap<QString, const t_eph*>;
95 }
96
97 // RINEX writer
98 // ------------
99 if (!rnxFileName.isEmpty()) {
100 _rnx = new bncClockRinex(rnxFileName, intr, samplClkRnx);
101 }
102 else {
103 _rnx = 0;
104 }
105
106 // SP3 writer
107 // ----------
108 if (!sp3FileName.isEmpty()) {
109 _sp3 = new bncSP3(sp3FileName, intr, samplSp3);
110 }
111 else {
112 _sp3 = 0;
113 }
114
115 // Set Transformation Parameters
116 // -----------------------------
117 // Transformation Parameters from ITRF2014 to ETRF2000
118 // EUREF Technical Note 1 Relationship and Transformation between the ITRF and ETRF
119 // Zuheir Altamimi, June 28, 2018
120 if (_crdTrafo == "ETRF2000") {
121 _dx = 0.0547;
122 _dy = 0.0522;
123 _dz = -0.0741;
124
125 _dxr = 0.0001;
126 _dyr = 0.0001;
127 _dzr = -0.0019;
128
129 _ox = 0.001701;
130 _oy = 0.010290;
131 _oz = -0.016632;
132
133 _oxr = 0.000081;
134 _oyr = 0.000490;
135 _ozr = -0.000729;
136
137 _sc = 2.12;
138 _scr = 0.11;
139
140 _t0 = 2010.0;
141 }
142 // Transformation Parameters from ITRF2014 to GDA2020 (Ryan Ruddick, GA)
143 else if (_crdTrafo == "GDA2020") {
144 _dx = 0.0;
145 _dy = 0.0;
146 _dz = 0.0;
147
148 _dxr = 0.0;
149 _dyr = 0.0;
150 _dzr = 0.0;
151
152 _ox = 0.0;
153 _oy = 0.0;
154 _oz = 0.0;
155
156 _oxr = 0.00150379;
157 _oyr = 0.00118346;
158 _ozr = 0.00120716;
159
160 _sc = 0.0;
161 _scr = 0.0;
162
163 _t0 = 2020.0;
164 }
165 // Transformation Parameters from IGb14 to SIRGAS2000 (Thanks to Sonia Costa, BRA)
166 // June 29 2020: TX:-0.0027 m TY:-0.0025 m TZ:-0.0042 m SCL:1.20 (ppb) no rotations and no rates.*/
167 else if (_crdTrafo == "SIRGAS2000") {
168 _dx = -0.0027;
169 _dy = -0.0025;
170 _dz = -0.0042;
171
172 _dxr = 0.0000;
173 _dyr = 0.0000;
174 _dzr = 0.0000;
175
176 _ox = 0.000000;
177 _oy = 0.000000;
178 _oz = 0.000000;
179
180 _oxr = 0.000000;
181 _oyr = 0.000000;
182 _ozr = 0.000000;
183
184 _sc = 1.20000;
185 _scr = 0.00000;
186 _t0 = 2000.0;
187 }
188 // Transformation Parameters from ITRF2014 to DREF91
189 else if (_crdTrafo == "DREF91") {
190 _dx = 0.0547;
191 _dy = 0.0522;
192 _dz = -0.0741;
193
194 _dxr = 0.0001;
195 _dyr = 0.0001;
196 _dzr = -0.0019;
197 // ERTF200 + rotation parameters (ETRF200 => DREF91)
198 _ox = 0.001701 + 0.000658;
199 _oy = 0.010290 - 0.000208;
200 _oz = -0.016632 + 0.000755;
201
202 _oxr = 0.000081;
203 _oyr = 0.000490;
204 _ozr = -0.000729;
205
206 _sc = 2.12;
207 _scr = 0.11;
208
209 _t0 = 2010.0;
210 }
211 else if (_crdTrafo == "Custom") {
212 _dx = settings.value("trafo_dx").toDouble();
213 _dy = settings.value("trafo_dy").toDouble();
214 _dz = settings.value("trafo_dz").toDouble();
215 _dxr = settings.value("trafo_dxr").toDouble();
216 _dyr = settings.value("trafo_dyr").toDouble();
217 _dzr = settings.value("trafo_dzr").toDouble();
218 _ox = settings.value("trafo_ox").toDouble();
219 _oy = settings.value("trafo_oy").toDouble();
220 _oz = settings.value("trafo_oz").toDouble();
221 _oxr = settings.value("trafo_oxr").toDouble();
222 _oyr = settings.value("trafo_oyr").toDouble();
223 _ozr = settings.value("trafo_ozr").toDouble();
224 _sc = settings.value("trafo_sc").toDouble();
225 _scr = settings.value("trafo_scr").toDouble();
226 _t0 = settings.value("trafo_t0").toDouble();
227 }
228}
229
230// Destructor
231////////////////////////////////////////////////////////////////////////////
232bncRtnetUploadCaster::~bncRtnetUploadCaster() {
233 if (isRunning()) {
234 wait();
235 }
236 delete _rnx;
237 delete _sp3;
238 delete _ephUser;
239 delete _usedEph;
240 delete _ssrCorr;
241}
242
243//
244////////////////////////////////////////////////////////////////////////////
245void bncRtnetUploadCaster::decodeRtnetStream(char* buffer, int bufLen) {
246
247 QMutexLocker locker(&_mutex);
248
249 // Append to internal buffer
250 // -------------------------
251 _rtnetStreamBuffer.append(QByteArray(buffer, bufLen));
252
253 // Select buffer part that contains last epoch
254 // -------------------------------------------
255 QStringList lines;
256 int iEpoBeg = _rtnetStreamBuffer.lastIndexOf('*'); // begin of last epoch
257 if (iEpoBeg == -1) {
258 _rtnetStreamBuffer.clear();
259 return;
260 }
261 int iEpoBegEarlier = _rtnetStreamBuffer.indexOf('*');
262 if (iEpoBegEarlier != -1 && iEpoBegEarlier < iEpoBeg) { // are there two epoch lines in buffer?
263 _rtnetStreamBuffer = _rtnetStreamBuffer.mid(iEpoBegEarlier);
264 }
265 else {
266 _rtnetStreamBuffer = _rtnetStreamBuffer.mid(iEpoBeg);
267 }
268 int iEpoEnd = _rtnetStreamBuffer.lastIndexOf("EOE"); // end of last epoch
269 if (iEpoEnd == -1) {
270 return;
271 }
272
273 while (_rtnetStreamBuffer.count('*') > 1) { // is there more than 1 epoch line in buffer?
274 QString rtnetStreamBuffer = _rtnetStreamBuffer.mid(1);
275 int nextEpoch = rtnetStreamBuffer.indexOf('*');
276 if (nextEpoch != -1 && nextEpoch < iEpoEnd) {
277 _rtnetStreamBuffer = _rtnetStreamBuffer.mid(nextEpoch);
278 }
279 else if (nextEpoch != -1 && nextEpoch >= iEpoEnd) {
280 break;
281 }
282 }
283
284 lines = _rtnetStreamBuffer.left(iEpoEnd).split('\n',
285 QString::SkipEmptyParts);
286 _rtnetStreamBuffer = _rtnetStreamBuffer.mid(iEpoEnd + 3);
287
288 if (lines.size() < 2) {
289 return;
290 }
291
292 // Read first line (with epoch time)
293 // ---------------------------------
294 QTextStream in(lines[0].toLatin1());
295 QString hlp;
296 int year, month, day, hour, min;
297 double sec;
298 in >> hlp >> year >> month >> day >> hour >> min >> sec;
299 bncTime epoTime;
300 epoTime.set(year, month, day, hour, min, sec);
301
302 emit(newMessage(
303 "bncRtnetUploadCaster: decode " + QByteArray(epoTime.datestr().c_str())
304 + " " + QByteArray(epoTime.timestr().c_str()) + " "
305 + _casterID.toLatin1(), false));
306
307 struct SsrCorr::ClockOrbit co;
308 memset(&co, 0, sizeof(co));
309 co.EpochTime[CLOCKORBIT_SATGPS] = static_cast<int>(epoTime.gpssec());
310 if (_ssrFormat == "RTCM-SSR") {
311 double gt = epoTime.gpssec() + 3 * 3600 - gnumleap(year, month, day);
312 co.EpochTime[CLOCKORBIT_SATGLONASS] = static_cast<int>(fmod(gt, 86400.0));
313 }
314 else if (_ssrFormat == "IGS-SSR") {
315 co.EpochTime[CLOCKORBIT_SATGLONASS] = static_cast<int>(epoTime.gpssec());
316 }
317 co.EpochTime[CLOCKORBIT_SATGALILEO] = static_cast<int>(epoTime.gpssec());
318 co.EpochTime[CLOCKORBIT_SATQZSS] = static_cast<int>(epoTime.gpssec());
319 co.EpochTime[CLOCKORBIT_SATSBAS] = static_cast<int>(epoTime.gpssec());
320 if (_ssrFormat == "RTCM-SSR") {
321 co.EpochTime[CLOCKORBIT_SATBDS] = static_cast<int>(epoTime.bdssec());
322 }
323 else if (_ssrFormat == "IGS-SSR") {
324 co.EpochTime[CLOCKORBIT_SATBDS] = static_cast<int>(epoTime.gpssec());
325 }
326 co.Supplied[_ssrCorr->COBOFS_CLOCK] = 1;
327 co.Supplied[_ssrCorr->COBOFS_ORBIT] = 1;
328 co.SatRefDatum = _ssrCorr->DATUM_ITRF; // ToDo: to decode from RTNET format
329 co.SSRIOD = _IOD;
330 co.SSRProviderID = _PID; // 256 .. BKG, 257 ... EUREF
331 co.SSRSolutionID = _SID;
332
333 struct SsrCorr::CodeBias bias;
334 memset(&bias, 0, sizeof(bias));
335 bias.EpochTime[CLOCKORBIT_SATGPS] = co.EpochTime[CLOCKORBIT_SATGPS];
336 bias.EpochTime[CLOCKORBIT_SATGLONASS] = co.EpochTime[CLOCKORBIT_SATGLONASS];
337 bias.EpochTime[CLOCKORBIT_SATGALILEO] = co.EpochTime[CLOCKORBIT_SATGALILEO];
338 bias.EpochTime[CLOCKORBIT_SATQZSS] = co.EpochTime[CLOCKORBIT_SATQZSS];
339 bias.EpochTime[CLOCKORBIT_SATSBAS] = co.EpochTime[CLOCKORBIT_SATSBAS];
340 bias.EpochTime[CLOCKORBIT_SATBDS] = co.EpochTime[CLOCKORBIT_SATBDS];
341 bias.SSRIOD = _IOD;
342 bias.SSRProviderID = _PID;
343 bias.SSRSolutionID = _SID;
344
345 struct SsrCorr::PhaseBias phasebias;
346 memset(&phasebias, 0, sizeof(phasebias));
347 unsigned int dispersiveBiasConsistenyIndicator = 0;
348 unsigned int mwConsistencyIndicator = 0;
349 phasebias.EpochTime[CLOCKORBIT_SATGPS] = co.EpochTime[CLOCKORBIT_SATGPS];
350 phasebias.EpochTime[CLOCKORBIT_SATGLONASS] = co.EpochTime[CLOCKORBIT_SATGLONASS];
351 phasebias.EpochTime[CLOCKORBIT_SATGALILEO] = co.EpochTime[CLOCKORBIT_SATGALILEO];
352 phasebias.EpochTime[CLOCKORBIT_SATQZSS] = co.EpochTime[CLOCKORBIT_SATQZSS];
353 phasebias.EpochTime[CLOCKORBIT_SATSBAS] = co.EpochTime[CLOCKORBIT_SATSBAS];
354 phasebias.EpochTime[CLOCKORBIT_SATBDS] = co.EpochTime[CLOCKORBIT_SATBDS];
355 phasebias.SSRIOD = _IOD;
356 phasebias.SSRProviderID = _PID;
357 phasebias.SSRSolutionID = _SID;
358
359 struct SsrCorr::VTEC vtec;
360 memset(&vtec, 0, sizeof(vtec));
361 vtec.EpochTime = static_cast<int>(epoTime.gpssec());
362 vtec.SSRIOD = _IOD;
363 vtec.SSRProviderID = _PID;
364 vtec.SSRSolutionID = _SID;
365
366 // Default Update Interval
367 // -----------------------
368 int clkUpdInd = 2; // 5 sec
369 int ephUpdInd = clkUpdInd; // default
370
371 if (_samplRtcmClkCorr > 5.0 && _samplRtcmEphCorr <= 5.0) { // combined orb and clock
372 ephUpdInd = determineUpdateInd(_samplRtcmClkCorr);
373 }
374 if (_samplRtcmClkCorr > 5.0) {
375 clkUpdInd = determineUpdateInd(_samplRtcmClkCorr);
376 }
377 if (_samplRtcmEphCorr > 5.0) {
378 ephUpdInd = determineUpdateInd(_samplRtcmEphCorr);
379 }
380
381 co.UpdateInterval = clkUpdInd;
382 bias.UpdateInterval = ephUpdInd;
383 phasebias.UpdateInterval = ephUpdInd;
384
385 for (int ii = 1; ii < lines.size(); ii++) {
386 QString key; // prn or key VTEC, IND (phase bias indicators)
387 double rtnUra = 0.0; // [m]
388 ColumnVector rtnAPC; rtnAPC.ReSize(3); rtnAPC = 0.0; // [m, m, m]
389 ColumnVector rtnVel; rtnVel.ReSize(3); rtnVel = 0.0; // [m/s, m/s, m/s]
390 ColumnVector rtnCoM; rtnCoM.ReSize(3); rtnCoM = 0.0; // [m, m, m]
391 ColumnVector rtnClk; rtnClk.ReSize(3); rtnClk = 0.0; // [m, m/s, m/s²]
392 ColumnVector rtnClkSig; rtnClkSig.ReSize(3); rtnClkSig = 0.0; // [m, m/s, m/s²]
393 t_prn prn;
394
395 QTextStream in(lines[ii].toLatin1());
396
397 in >> key;
398
399 // non-satellite specific parameters
400 if (key.contains("IND", Qt::CaseSensitive)) {
401 in >> dispersiveBiasConsistenyIndicator >> mwConsistencyIndicator;
402 continue;
403 }
404 // non-satellite specific parameters
405 if (key.contains("VTEC", Qt::CaseSensitive)) {
406 double ui;
407 in >> ui >> vtec.NumLayers;
408 vtec.UpdateInterval = (unsigned int) determineUpdateInd(ui);
409 for (unsigned ll = 0; ll < vtec.NumLayers; ll++) {
410 int dummy;
411 in >> dummy >> vtec.Layers[ll].Degree >> vtec.Layers[ll].Order
412 >> vtec.Layers[ll].Height;
413 for (unsigned iDeg = 0; iDeg <= vtec.Layers[ll].Degree; iDeg++) {
414 for (unsigned iOrd = 0; iOrd <= vtec.Layers[ll].Order; iOrd++) {
415 in >> vtec.Layers[ll].Cosinus[iDeg][iOrd];
416 }
417 }
418 for (unsigned iDeg = 0; iDeg <= vtec.Layers[ll].Degree; iDeg++) {
419 for (unsigned iOrd = 0; iOrd <= vtec.Layers[ll].Order; iOrd++) {
420 in >> vtec.Layers[ll].Sinus[iDeg][iOrd];
421 }
422 }
423 }
424 continue;
425 }
426 // satellite specific parameters
427 char sys = key.mid(0, 1).at(0).toLatin1();
428 int number = key.mid(1, 2).toInt();
429 int flags = 0;
430 if (sys == 'E') { // I/NAV
431 flags = 1;
432 }
433 prn.set(sys, number, flags);
434 QString prnInternalStr = QString::fromStdString(prn.toInternalString());
435 QString prnStr = QString::fromStdString(prn.toString());
436
437 const t_eph* ephLast = _ephUser->ephLast(prnInternalStr);
438 const t_eph* ephPrev = _ephUser->ephPrev(prnInternalStr);
439 const t_eph* eph = ephLast;
440 if (eph) {
441
442 // Use previous ephemeris if the last one is too recent
443 // ----------------------------------------------------
444 const int MINAGE = 60; // seconds
445 if (ephPrev && eph->receptDateTime().isValid()
446 && eph->receptDateTime().secsTo(currentDateAndTimeGPS()) < MINAGE) {
447 eph = ephPrev;
448 }
449
450 // Make sure the clock messages refer to same IOD as orbit messages
451 // ----------------------------------------------------------------
452 if (_usedEph) {
453 if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
454 (*_usedEph)[prnInternalStr] = eph;
455 }
456 else {
457 eph = 0;
458 if (_usedEph->contains(prnInternalStr)) {
459 const t_eph* usedEph = _usedEph->value(prnInternalStr);
460 if (usedEph == ephLast) {
461 eph = ephLast;
462 }
463 else if (usedEph == ephPrev) {
464 eph = ephPrev;
465 }
466 }
467 }
468 }
469 }
470
471 if (eph &&
472 eph->checkState() != t_eph::bad &&
473 eph->checkState() != t_eph::unhealthy &&
474 eph->checkState() != t_eph::outdated) {
475 QMap<QString, double> codeBiases;
476 QList<phaseBiasSignal> phaseBiasList;
477 phaseBiasesSat pbSat;
478 _phaseBiasInformationDecoded = false;
479
480 while (true) {
481 QString key;
482 int numVal = 0;
483 in >> key;
484 if (in.status() != QTextStream::Ok) {
485 break;
486 }
487 if (key == "APC") {
488 in >> numVal;
489 rtnAPC.ReSize(3); rtnAPC = 0.0;
490 for (int ii = 0; ii < numVal; ii++) {
491 in >> rtnAPC[ii];
492 }
493 }
494 else if (key == "Ura") {
495 in >> numVal;
496 if (numVal == 1)
497 in >> rtnUra;
498 }
499 else if (key == "Clk") {
500 in >> numVal;
501 rtnClk.ReSize(3); rtnClk = 0.0;
502 for (int ii = 0; ii < numVal; ii++) {
503 in >> rtnClk[ii];
504 }
505 }
506 else if (key == "ClkSig") {
507 in >> numVal;
508 rtnClkSig.ReSize(3); rtnClkSig = 0.0;
509 for (int ii = 0; ii < numVal; ii++) {
510 in >> rtnClkSig[ii];
511 }
512 }
513 else if (key == "Vel") {
514 in >> numVal;
515 rtnVel.ReSize(3); rtnVel = 0.0;
516 for (int ii = 0; ii < numVal; ii++) {
517 in >> rtnVel[ii];
518 }
519 }
520 else if (key == "CoM") {
521 in >> numVal;
522 rtnCoM.ReSize(3); rtnCoM = 0.0;
523 for (int ii = 0; ii < numVal; ii++) {
524 in >> rtnCoM[ii];
525 }
526 }
527 else if (key == "CodeBias") {
528 in >> numVal;
529 for (int ii = 0; ii < numVal; ii++) {
530 QString type;
531 double value;
532 in >> type >> value;
533 codeBiases[type] = value;
534 }
535 }
536 else if (key == "YawAngle") {
537 _phaseBiasInformationDecoded = true;
538 in >> numVal >> pbSat.yawAngle;
539 if (pbSat.yawAngle < 0.0) {
540 pbSat.yawAngle += (2*M_PI);
541 }
542 else if (pbSat.yawAngle > 2*M_PI) {
543 pbSat.yawAngle -= (2*M_PI);
544 }
545 }
546 else if (key == "YawRate") {
547 _phaseBiasInformationDecoded = true;
548 in >> numVal >> pbSat.yawRate;
549 }
550 else if (key == "PhaseBias") {
551 _phaseBiasInformationDecoded = true;
552 in >> numVal;
553 for (int ii = 0; ii < numVal; ii++) {
554 phaseBiasSignal pb;
555 in >> pb.type >> pb.bias >> pb.integerIndicator
556 >> pb.wlIndicator >> pb.discontinuityCounter;
557 phaseBiasList.append(pb);
558 }
559 }
560 else {
561 in >> numVal;
562 for (int ii = 0; ii < numVal; ii++) {
563 double dummy;
564 in >> dummy;
565 }
566 emit(newMessage(" RTNET format error: "
567 + lines[ii].toLatin1(), false));
568 }
569 }
570
571 struct SsrCorr::ClockOrbit::SatData* sd = 0;
572 if (prn.system() == 'G') {
573 sd = co.Sat + co.NumberOfSat[CLOCKORBIT_SATGPS];
574 ++co.NumberOfSat[CLOCKORBIT_SATGPS];
575 }
576 else if (prn.system() == 'R') {
577 sd = co.Sat + CLOCKORBIT_NUMGPS + co.NumberOfSat[CLOCKORBIT_SATGLONASS];
578 ++co.NumberOfSat[CLOCKORBIT_SATGLONASS];
579 }
580 else if (prn.system() == 'E') {
581 sd = co.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
582 + co.NumberOfSat[CLOCKORBIT_SATGALILEO];
583 ++co.NumberOfSat[CLOCKORBIT_SATGALILEO];
584 }
585 else if (prn.system() == 'J') {
586 sd = co.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
587 + CLOCKORBIT_NUMGALILEO
588 + co.NumberOfSat[CLOCKORBIT_SATQZSS];
589 ++co.NumberOfSat[CLOCKORBIT_SATQZSS];
590 }
591 else if (prn.system() == 'S') {
592 sd = co.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
593 + CLOCKORBIT_NUMGALILEO + CLOCKORBIT_NUMQZSS
594 + co.NumberOfSat[CLOCKORBIT_SATSBAS];
595 ++co.NumberOfSat[CLOCKORBIT_SATSBAS];
596 }
597 else if (prn.system() == 'C') {
598 sd = co.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
599 + CLOCKORBIT_NUMGALILEO + CLOCKORBIT_NUMQZSS
600 + CLOCKORBIT_NUMSBAS
601 + co.NumberOfSat[CLOCKORBIT_SATBDS];
602 ++co.NumberOfSat[CLOCKORBIT_SATBDS];
603 }
604 if (sd) {
605 QString outLine;
606 t_irc irc = processSatellite(eph, epoTime.gpsw(), epoTime.gpssec(), prnStr, rtnAPC,
607 rtnUra, rtnClk, rtnVel, rtnCoM, rtnClkSig, sd, outLine);
608 if (irc != success) {/*
609 // very few cases: check states bad and unhealthy are excluded earlier
610 sd->ID = prnStr.mid(1).toInt(); // to prevent G00, R00 entries
611 sd->IOD = eph->IOD();
612 */
613 continue;
614 }
615 }
616
617 // Code Biases
618 // -----------
619 struct SsrCorr::CodeBias::BiasSat* biasSat = 0;
620 if (!codeBiases.isEmpty()) {
621 if (prn.system() == 'G') {
622 biasSat = bias.Sat + bias.NumberOfSat[CLOCKORBIT_SATGPS];
623 ++bias.NumberOfSat[CLOCKORBIT_SATGPS];
624 }
625 else if (prn.system() == 'R') {
626 biasSat = bias.Sat + CLOCKORBIT_NUMGPS
627 + bias.NumberOfSat[CLOCKORBIT_SATGLONASS];
628 ++bias.NumberOfSat[CLOCKORBIT_SATGLONASS];
629 }
630 else if (prn.system() == 'E') {
631 biasSat = bias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
632 + bias.NumberOfSat[CLOCKORBIT_SATGALILEO];
633 ++bias.NumberOfSat[CLOCKORBIT_SATGALILEO];
634 }
635 else if (prn.system() == 'J') {
636 biasSat = bias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
637 + CLOCKORBIT_NUMGALILEO
638 + bias.NumberOfSat[CLOCKORBIT_SATQZSS];
639 ++bias.NumberOfSat[CLOCKORBIT_SATQZSS];
640 }
641 else if (prn.system() == 'S') {
642 biasSat = bias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
643 + CLOCKORBIT_NUMGALILEO + CLOCKORBIT_NUMQZSS
644 + bias.NumberOfSat[CLOCKORBIT_SATSBAS];
645 ++bias.NumberOfSat[CLOCKORBIT_SATSBAS];
646 }
647 else if (prn.system() == 'C') {
648 biasSat = bias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
649 + CLOCKORBIT_NUMGALILEO + CLOCKORBIT_NUMQZSS
650 + CLOCKORBIT_NUMSBAS
651 + bias.NumberOfSat[CLOCKORBIT_SATBDS];
652 ++bias.NumberOfSat[CLOCKORBIT_SATBDS];
653 }
654 }
655
656 if (biasSat) {
657 biasSat->ID = prn.number();
658 biasSat->NumberOfCodeBiases = 0;
659 QMapIterator<QString, double> it(codeBiases);
660 while (it.hasNext()) {
661 it.next();
662 int ii = biasSat->NumberOfCodeBiases;
663 if (ii >= CLOCKORBIT_NUMBIAS)
664 break;
665 SsrCorr::CodeType type = _ssrCorr->rnxTypeToCodeType(prn.system(), it.key().toStdString());
666 if (type != _ssrCorr->RESERVED) {
667 biasSat->NumberOfCodeBiases += 1;
668 biasSat->Biases[ii].Type = type;
669 biasSat->Biases[ii].Bias = it.value();
670 }
671 }
672 }
673
674 // Phase Biases
675 // ------------
676 struct SsrCorr::PhaseBias::PhaseBiasSat* phasebiasSat = 0;
677 if (prn.system() == 'G') {
678 phasebiasSat = phasebias.Sat
679 + phasebias.NumberOfSat[CLOCKORBIT_SATGPS];
680 ++phasebias.NumberOfSat[CLOCKORBIT_SATGPS];
681 }
682 else if (prn.system() == 'R') {
683 phasebiasSat = phasebias.Sat + CLOCKORBIT_NUMGPS
684 + phasebias.NumberOfSat[CLOCKORBIT_SATGLONASS];
685 ++phasebias.NumberOfSat[CLOCKORBIT_SATGLONASS];
686 }
687 else if (prn.system() == 'E') {
688 phasebiasSat = phasebias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
689 + phasebias.NumberOfSat[CLOCKORBIT_SATGALILEO];
690 ++phasebias.NumberOfSat[CLOCKORBIT_SATGALILEO];
691 }
692 else if (prn.system() == 'J') {
693 phasebiasSat = phasebias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
694 + CLOCKORBIT_NUMGALILEO
695 + phasebias.NumberOfSat[CLOCKORBIT_SATQZSS];
696 ++phasebias.NumberOfSat[CLOCKORBIT_SATQZSS];
697 }
698 else if (prn.system() == 'S') {
699 phasebiasSat = phasebias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
700 + CLOCKORBIT_NUMGALILEO + CLOCKORBIT_NUMQZSS
701 + phasebias.NumberOfSat[CLOCKORBIT_SATSBAS];
702 ++phasebias.NumberOfSat[CLOCKORBIT_SATSBAS];
703 }
704 else if (prn.system() == 'C') {
705 phasebiasSat = phasebias.Sat + CLOCKORBIT_NUMGPS + CLOCKORBIT_NUMGLONASS
706 + CLOCKORBIT_NUMGALILEO + CLOCKORBIT_NUMQZSS
707 + CLOCKORBIT_NUMSBAS
708 + phasebias.NumberOfSat[CLOCKORBIT_SATBDS];
709 ++phasebias.NumberOfSat[CLOCKORBIT_SATBDS];
710 }
711
712 if (phasebiasSat && _phaseBiasInformationDecoded) {
713 phasebias.DispersiveBiasConsistencyIndicator = dispersiveBiasConsistenyIndicator;
714 phasebias.MWConsistencyIndicator = mwConsistencyIndicator;
715 phasebiasSat->ID = prn.number();
716 phasebiasSat->NumberOfPhaseBiases = 0;
717 phasebiasSat->YawAngle = pbSat.yawAngle;
718 phasebiasSat->YawRate = pbSat.yawRate;
719 QListIterator<phaseBiasSignal> it(phaseBiasList);
720 while (it.hasNext()) {
721 const phaseBiasSignal &pbSig = it.next();
722 int ii = phasebiasSat->NumberOfPhaseBiases;
723 if (ii >= CLOCKORBIT_NUMBIAS)
724 break;
725 SsrCorr::CodeType type = _ssrCorr->rnxTypeToCodeType(prn.system(), pbSig.type.toStdString());
726 if (type != _ssrCorr->RESERVED) {
727 phasebiasSat->NumberOfPhaseBiases += 1;
728 phasebiasSat->Biases[ii].Type = type;
729 phasebiasSat->Biases[ii].Bias = pbSig.bias;
730 phasebiasSat->Biases[ii].SignalIntegerIndicator = pbSig.integerIndicator;
731 phasebiasSat->Biases[ii].SignalsWideLaneIntegerIndicator = pbSig.wlIndicator;
732 phasebiasSat->Biases[ii].SignalDiscontinuityCounter = pbSig.discontinuityCounter;
733 }
734 }
735 }
736 }
737 }
738
739 QByteArray hlpBufferCo;
740
741 // Orbit and Clock Corrections together
742 // ------------------------------------
743 if (_samplRtcmEphCorr == 0.0) {
744 if (co.NumberOfSat[CLOCKORBIT_SATGPS] > 0
745 || co.NumberOfSat[CLOCKORBIT_SATGLONASS] > 0
746 || co.NumberOfSat[CLOCKORBIT_SATGALILEO] > 0
747 || co.NumberOfSat[CLOCKORBIT_SATQZSS] > 0
748 || co.NumberOfSat[CLOCKORBIT_SATSBAS] > 0
749 || co.NumberOfSat[CLOCKORBIT_SATBDS] > 0) {
750 char obuffer[CLOCKORBIT_BUFFERSIZE];
751 int len = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_AUTO, 0, obuffer, sizeof(obuffer));
752 if (len > 0) {
753 hlpBufferCo = QByteArray(obuffer, len);
754 }
755 }
756 }
757
758 // Orbit and Clock Corrections separately
759 // --------------------------------------
760 else {
761 if (co.NumberOfSat[CLOCKORBIT_SATGPS] > 0) {
762 char obuffer[CLOCKORBIT_BUFFERSIZE];
763 if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
764 co.UpdateInterval = ephUpdInd;
765 int len1 = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_GPSORBIT, 1, obuffer,
766 sizeof(obuffer));
767 co.UpdateInterval = clkUpdInd;
768 if (len1 > 0) {
769 hlpBufferCo += QByteArray(obuffer, len1);
770 }
771 }
772 int mmsg = (co.NumberOfSat[CLOCKORBIT_SATGLONASS] > 0 ||
773 co.NumberOfSat[CLOCKORBIT_SATGALILEO] > 0 ||
774 co.NumberOfSat[CLOCKORBIT_SATQZSS] > 0 ||
775 co.NumberOfSat[CLOCKORBIT_SATSBAS] > 0 ||
776 co.NumberOfSat[CLOCKORBIT_SATBDS] > 0 ) ? 1 : 0;
777 int len2 = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_GPSCLOCK, mmsg, obuffer,
778 sizeof(obuffer));
779 if (len2 > 0) {
780 hlpBufferCo += QByteArray(obuffer, len2);
781 }
782 }
783 if (co.NumberOfSat[CLOCKORBIT_SATGLONASS] > 0) {
784 char obuffer[CLOCKORBIT_BUFFERSIZE];
785 if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
786 co.UpdateInterval = ephUpdInd;
787 int len1 = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_GLONASSORBIT, 1, obuffer,
788 sizeof(obuffer));
789 co.UpdateInterval = clkUpdInd;
790 if (len1 > 0) {
791 hlpBufferCo += QByteArray(obuffer, len1);
792 }
793 }
794 int mmsg = (co.NumberOfSat[CLOCKORBIT_SATGALILEO] > 0 ||
795 co.NumberOfSat[CLOCKORBIT_SATQZSS] > 0 ||
796 co.NumberOfSat[CLOCKORBIT_SATSBAS] > 0 ||
797 co.NumberOfSat[CLOCKORBIT_SATBDS] > 0 ) ? 1 : 0;
798 int len2 = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_GLONASSCLOCK, mmsg, obuffer,
799 sizeof(obuffer));
800 if (len2 > 0) {
801 hlpBufferCo += QByteArray(obuffer, len2);
802 }
803 }
804 if (co.NumberOfSat[CLOCKORBIT_SATGALILEO] > 0) {
805 char obuffer[CLOCKORBIT_BUFFERSIZE];
806 if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
807 co.UpdateInterval = ephUpdInd;
808 int len1 = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_GALILEOORBIT, 1, obuffer,
809 sizeof(obuffer));
810 co.UpdateInterval = clkUpdInd;
811 if (len1 > 0) {
812 hlpBufferCo += QByteArray(obuffer, len1);
813 }
814 }
815 int mmsg = (co.NumberOfSat[CLOCKORBIT_SATQZSS] > 0 ||
816 co.NumberOfSat[CLOCKORBIT_SATSBAS] > 0 ||
817 co.NumberOfSat[CLOCKORBIT_SATBDS] > 0 ) ? 1 : 0;
818 int len2 = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_GALILEOCLOCK, mmsg, obuffer,
819 sizeof(obuffer));
820 if (len2 > 0) {
821 hlpBufferCo += QByteArray(obuffer, len2);
822 }
823 }
824 if (co.NumberOfSat[CLOCKORBIT_SATQZSS] > 0) {
825 char obuffer[CLOCKORBIT_BUFFERSIZE];
826 if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
827 co.UpdateInterval = ephUpdInd;
828 int len1 = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_QZSSORBIT, 1, obuffer,
829 sizeof(obuffer));
830 co.UpdateInterval = clkUpdInd;
831 if (len1 > 0) {
832 hlpBufferCo += QByteArray(obuffer, len1);
833 }
834 }
835 int mmsg = (co.NumberOfSat[CLOCKORBIT_SATSBAS] > 0 ||
836 co.NumberOfSat[CLOCKORBIT_SATBDS] > 0 ) ? 1 : 0;
837 int len2 = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_QZSSCLOCK, mmsg, obuffer,
838 sizeof(obuffer));
839 if (len2 > 0) {
840 hlpBufferCo += QByteArray(obuffer, len2);
841 }
842 }
843 if (co.NumberOfSat[CLOCKORBIT_SATSBAS] > 0) {
844 char obuffer[CLOCKORBIT_BUFFERSIZE];
845 if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
846 co.UpdateInterval = ephUpdInd;
847 int len1 = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_SBASORBIT, 1, obuffer,
848 sizeof(obuffer));
849 co.UpdateInterval = clkUpdInd;
850 if (len1 > 0) {
851 hlpBufferCo += QByteArray(obuffer, len1);
852 }
853 }
854 int mmsg = (co.NumberOfSat[CLOCKORBIT_SATBDS] > 0) ? 1 : 0;
855 int len2 = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_SBASCLOCK, mmsg, obuffer,
856 sizeof(obuffer));
857 if (len2 > 0) {
858 hlpBufferCo += QByteArray(obuffer, len2);
859 }
860 }
861 if (co.NumberOfSat[CLOCKORBIT_SATBDS] > 0) {
862 char obuffer[CLOCKORBIT_BUFFERSIZE];
863 if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
864 co.UpdateInterval = ephUpdInd;
865 int len1 = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_BDSORBIT, 1, obuffer,
866 sizeof(obuffer));
867 co.UpdateInterval = clkUpdInd;
868 if (len1 > 0) {
869 hlpBufferCo += QByteArray(obuffer, len1);
870 }
871 }
872 int mmsg = 0;
873 int len2 = _ssrCorr->MakeClockOrbit(&co, _ssrCorr->COTYPE_BDSCLOCK, mmsg, obuffer,
874 sizeof(obuffer));
875 if (len2 > 0) {
876 hlpBufferCo += QByteArray(obuffer, len2);
877 }
878 }
879 }
880
881 // Code Biases
882 // -----------
883 QByteArray hlpBufferBias;
884 if (bias.NumberOfSat[CLOCKORBIT_SATGPS] > 0
885 || bias.NumberOfSat[CLOCKORBIT_SATGLONASS] > 0
886 || bias.NumberOfSat[CLOCKORBIT_SATGALILEO] > 0
887 || bias.NumberOfSat[CLOCKORBIT_SATQZSS] > 0
888 || bias.NumberOfSat[CLOCKORBIT_SATSBAS] > 0
889 || bias.NumberOfSat[CLOCKORBIT_SATBDS] > 0) {
890 char obuffer[CLOCKORBIT_BUFFERSIZE];
891 if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
892 int len = _ssrCorr->MakeCodeBias(&bias, _ssrCorr->CBTYPE_AUTO, 0, obuffer, sizeof(obuffer));
893 if (len > 0) {
894 hlpBufferBias = QByteArray(obuffer, len);
895 }
896 }
897 }
898
899 // Phase Biases
900 // ------------
901 QByteArray hlpBufferPhaseBias;
902 if ((phasebias.NumberOfSat[CLOCKORBIT_SATGPS] > 0
903 || phasebias.NumberOfSat[CLOCKORBIT_SATGLONASS] > 0
904 || phasebias.NumberOfSat[CLOCKORBIT_SATGALILEO] > 0
905 || phasebias.NumberOfSat[CLOCKORBIT_SATQZSS] > 0
906 || phasebias.NumberOfSat[CLOCKORBIT_SATSBAS] > 0
907 || phasebias.NumberOfSat[CLOCKORBIT_SATBDS] > 0)
908 && (_phaseBiasInformationDecoded)) {
909 char obuffer[CLOCKORBIT_BUFFERSIZE];
910 if (fmod(epoTime.gpssec(), _samplRtcmEphCorr) == 0.0) {
911 int len = _ssrCorr->MakePhaseBias(&phasebias, _ssrCorr->PBTYPE_AUTO, 0, obuffer, sizeof(obuffer));
912 if (len > 0) {
913 hlpBufferPhaseBias = QByteArray(obuffer, len);
914 }
915 }
916 }
917
918 // VTEC
919 // ----
920 QByteArray hlpBufferVtec;
921 if (vtec.NumLayers > 0) {
922 char obuffer[CLOCKORBIT_BUFFERSIZE];
923 int len = _ssrCorr->MakeVTEC(&vtec, 0, obuffer, sizeof(obuffer));
924 if (len > 0) {
925 hlpBufferVtec = QByteArray(obuffer, len);
926 }
927 }
928
929 _outBuffer += hlpBufferCo + hlpBufferBias + hlpBufferPhaseBias
930 + hlpBufferVtec;
931}
932
933//
934////////////////////////////////////////////////////////////////////////////
935t_irc bncRtnetUploadCaster::processSatellite(const t_eph* eph, int GPSweek,
936 double GPSweeks, const QString& prn, const ColumnVector& rtnAPC,
937 double rtnUra, const ColumnVector& rtnClk, const ColumnVector& rtnVel,
938 const ColumnVector& rtnCoM, const ColumnVector& rtnClkSig,
939 struct SsrCorr::ClockOrbit::SatData* sd, QString& outLine) {
940
941 // Broadcast Position and Velocity
942 // -------------------------------
943 ColumnVector xB(6);
944 ColumnVector vB(3);
945 t_irc irc = eph->getCrd(bncTime(GPSweek, GPSweeks), xB, vB, false);
946
947 if (irc != success) {
948 return irc;
949 }
950
951 // Precise Position
952 // ----------------
953 ColumnVector xP = _CoM ? rtnCoM : rtnAPC;
954
955 if (xP.size() == 0) {
956 return failure;
957 }
958
959 double dc = 0.0;
960 if (_crdTrafo != "IGS14") {
961 crdTrafo(GPSweek, xP, dc);
962 }
963
964 // Difference in xyz
965 // -----------------
966 ColumnVector dx = xB.Rows(1, 3) - xP;
967 ColumnVector dv = vB - rtnVel;
968
969 // Difference in RSW
970 // -----------------
971 ColumnVector rsw(3);
972 XYZ_to_RSW(xB.Rows(1, 3), vB, dx, rsw);
973
974 ColumnVector dotRsw(3);
975 XYZ_to_RSW(xB.Rows(1, 3), vB, dv, dotRsw);
976
977 // Clock Correction
978 // ----------------
979 double dClkA0 = rtnClk(1) - (xB(4) - dc) * t_CST::c;
980 double dClkA1 = 0.0;
981 if (rtnClk(2)) {
982 dClkA1 = rtnClk(2) - xB(5) * t_CST::c;
983 }
984 double dClkA2 = 0.0;
985 if (rtnClk(3)) {
986 dClkA2 = rtnClk(3) - xB(6) * t_CST::c;
987 }
988
989 if (sd) {
990 sd->ID = prn.mid(1).toInt();
991 sd->IOD = eph->IOD();
992 sd->Clock.DeltaA0 = dClkA0;
993 sd->Clock.DeltaA1 = dClkA1;
994 sd->Clock.DeltaA2 = dClkA2;
995 sd->UserRangeAccuracy = rtnUra;
996 sd->Orbit.DeltaRadial = rsw(1);
997 sd->Orbit.DeltaAlongTrack = rsw(2);
998 sd->Orbit.DeltaCrossTrack = rsw(3);
999 sd->Orbit.DotDeltaRadial = dotRsw(1);
1000 sd->Orbit.DotDeltaAlongTrack = dotRsw(2);
1001 sd->Orbit.DotDeltaCrossTrack = dotRsw(3);
1002
1003 if (corrIsOutOfRange(sd)) {
1004 return failure;
1005 }
1006 }
1007
1008 outLine.sprintf("%d %.1f %s %u %10.3f %8.3f %8.3f %8.3f %8.3f %8.3f\n", GPSweek,
1009 GPSweeks, eph->prn().toString().c_str(), eph->IOD(), dClkA0, dClkA1, dClkA2,
1010 rsw(1), rsw(2), rsw(3)); //fprintf(stderr, "%s\n", outLine.toStdString().c_str());
1011
1012 // RTNET full clock for RINEX and SP3 file
1013 // ---------------------------------------
1014 double relativity = -2.0 * DotProduct(xP, rtnVel) / t_CST::c;
1015 double clkRnx = (rtnClk[0] - relativity) / t_CST::c; // [s]
1016 double clkRnxRate = rtnClk[1] / t_CST::c; // [s/s = -]
1017 double clkRnxAcc = rtnClk[2] / t_CST::c; // [s/s² ) -/s]
1018
1019 if (_rnx) {
1020 double clkRnxSig, clkRnxRateSig, clkRnxAccSig;
1021 int s = rtnClkSig.size();
1022 switch (s) {
1023 case 1:
1024 clkRnxSig = rtnClkSig[0] / t_CST::c; // [s]
1025 clkRnxRateSig = 0.0; // [s/s = -]
1026 clkRnxAccSig = 0.0; // [s/s² ) -/s]
1027 break;
1028 case 2:
1029 clkRnxSig = rtnClkSig[0] / t_CST::c; // [s]
1030 clkRnxRateSig = rtnClkSig[1] / t_CST::c; // [s/s = -]
1031 clkRnxAccSig = 0.0; // [s/s² ) -/s]
1032 break;
1033 case 3:
1034 clkRnxSig = rtnClkSig[0] / t_CST::c; // [s]
1035 clkRnxRateSig = rtnClkSig[1] / t_CST::c; // [s/s = -]
1036 clkRnxAccSig = rtnClkSig[2] / t_CST::c; // [s/s² ) -/s]
1037 break;
1038 }
1039 _rnx->write(GPSweek, GPSweeks, prn, clkRnx, clkRnxRate, clkRnxAcc,
1040 clkRnxSig, clkRnxRateSig, clkRnxAccSig);
1041 }
1042 if (_sp3) {
1043 _sp3->write(GPSweek, GPSweeks, prn, rtnCoM, clkRnx, rtnVel, clkRnxRate);
1044 }
1045 return success;
1046}
1047
1048// Transform Coordinates
1049////////////////////////////////////////////////////////////////////////////
1050void bncRtnetUploadCaster::crdTrafo(int GPSWeek, ColumnVector& xyz,
1051 double& dc) {
1052
1053 // Current epoch minus 2000.0 in years
1054 // ------------------------------------
1055 double dt = (GPSWeek - (1042.0 + 6.0 / 7.0)) / 365.2422 * 7.0 + 2000.0 - _t0;
1056
1057 ColumnVector dx(3);
1058
1059 dx(1) = _dx + dt * _dxr;
1060 dx(2) = _dy + dt * _dyr;
1061 dx(3) = _dz + dt * _dzr;
1062
1063 static const double arcSec = 180.0 * 3600.0 / M_PI;
1064
1065 double ox = (_ox + dt * _oxr) / arcSec;
1066 double oy = (_oy + dt * _oyr) / arcSec;
1067 double oz = (_oz + dt * _ozr) / arcSec;
1068
1069 double sc = 1.0 + _sc * 1e-9 + dt * _scr * 1e-9;
1070
1071 // Specify approximate center of area
1072 // ----------------------------------
1073 ColumnVector meanSta(3);
1074
1075 if (_crdTrafo == "ETRF2000") {
1076 meanSta(1) = 3661090.0;
1077 meanSta(2) = 845230.0;
1078 meanSta(3) = 5136850.0;
1079 }
1080 else if (_crdTrafo == "GDA2020") {
1081 meanSta(1) = -4052050.0;
1082 meanSta(2) = 4212840.0;
1083 meanSta(3) = -2545110.0;
1084 }
1085 else if (_crdTrafo == "SIRGAS2000") {
1086 meanSta(1) = 3740860.0;
1087 meanSta(2) = -4964290.0;
1088 meanSta(3) = -1425420.0;
1089 }
1090 else if (_crdTrafo == "DREF91") {
1091 meanSta(1) = 3959579.0;
1092 meanSta(2) = 721719.0;
1093 meanSta(3) = 4931539.0;
1094 }
1095 else if (_crdTrafo == "Custom") {
1096 meanSta(1) = 0.0; // TODO
1097 meanSta(2) = 0.0; // TODO
1098 meanSta(3) = 0.0; // TODO
1099 }
1100
1101 // Clock correction proportional to topocentric distance to satellites
1102 // -------------------------------------------------------------------
1103 double rho = (xyz - meanSta).NormFrobenius();
1104 dc = rho * (sc - 1.0) / sc / t_CST::c;
1105
1106 Matrix rMat(3, 3);
1107 rMat(1, 1) = 1.0;
1108 rMat(1, 2) = -oz;
1109 rMat(1, 3) = oy;
1110 rMat(2, 1) = oz;
1111 rMat(2, 2) = 1.0;
1112 rMat(2, 3) = -ox;
1113 rMat(3, 1) = -oy;
1114 rMat(3, 2) = ox;
1115 rMat(3, 3) = 1.0;
1116
1117 xyz = sc * rMat * xyz + dx;
1118}
1119
1120int bncRtnetUploadCaster::determineUpdateInd(double samplingRate) {
1121
1122 if (samplingRate == 10.0) {
1123 return 3;
1124 }
1125 else if (samplingRate == 15.0) {
1126 return 4;
1127 }
1128 else if (samplingRate == 30.0) {
1129 return 5;
1130 }
1131 else if (samplingRate == 60.0) {
1132 return 6;
1133 }
1134 else if (samplingRate == 120.0) {
1135 return 7;
1136 }
1137 else if (samplingRate == 240.0) {
1138 return 8;
1139 }
1140 else if (samplingRate == 300.0) {
1141 return 9;
1142 }
1143 else if (samplingRate == 600.0) {
1144 return 10;
1145 }
1146 else if (samplingRate == 900.0) {
1147 return 11;
1148 }
1149 else if (samplingRate == 1800.0) {
1150 return 12;
1151 }
1152 else if (samplingRate == 3600.0) {
1153 return 13;
1154 }
1155 else if (samplingRate == 7200.0) {
1156 return 14;
1157 }
1158 else if (samplingRate == 10800.0) {
1159 return 15;
1160 }
1161 return 2; // default
1162}
1163
1164bool bncRtnetUploadCaster::corrIsOutOfRange(struct SsrCorr::ClockOrbit::SatData* sd) {
1165
1166 if (fabs(sd->Clock.DeltaA0) > 209.7151) {return true;}
1167 if (fabs(sd->Clock.DeltaA1) > 1.048575) {return true;}
1168 if (fabs(sd->Clock.DeltaA2) > 1.34217726) {return true;}
1169
1170 if (fabs(sd->Orbit.DeltaRadial) > 209.7151) {return true;}
1171 if (fabs(sd->Orbit.DeltaAlongTrack) > 209.7148) {return true;}
1172 if (fabs(sd->Orbit.DeltaCrossTrack) > 209.7148) {return true;}
1173
1174 if (fabs(sd->Orbit.DotDeltaRadial) > 1.048575) {return true;}
1175 if (fabs(sd->Orbit.DotDeltaAlongTrack) > 1.048572) {return true;}
1176 if (fabs(sd->Orbit.DotDeltaCrossTrack) > 1.048572) {return true;}
1177
1178 return false;
1179}
1180
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