source: ntrip/trunk/BNC/src/ephemeris.cpp@ 9774

Last change on this file since 9774 was 9774, checked in by stuerze, 8 weeks ago
File size: 54.4 KB
Line 
1#include <sstream>
2#include <iostream>
3#include <iomanip>
4#include <cstring>
5
6#include <newmatio.h>
7
8#include "ephemeris.h"
9#include "bncutils.h"
10#include "bnctime.h"
11#include "bnccore.h"
12#include "bncutils.h"
13#include "satObs.h"
14#include "pppInclude.h"
15#include "pppModel.h"
16
17using namespace std;
18
19// Constructor
20////////////////////////////////////////////////////////////////////////////
21t_eph::t_eph() {
22 _checkState = unchecked;
23 _navType = undefined;
24 _orbCorr = 0;
25 _clkCorr = 0;
26}
27// Destructor
28////////////////////////////////////////////////////////////////////////////
29t_eph::~t_eph() {
30 if (_orbCorr)
31 delete _orbCorr;
32 if (_clkCorr)
33 delete _clkCorr;
34}
35
36//
37////////////////////////////////////////////////////////////////////////////
38void t_eph::setOrbCorr(const t_orbCorr* orbCorr) {
39 if (_orbCorr) {
40 delete _orbCorr;
41 _orbCorr = 0;
42 }
43 _orbCorr = new t_orbCorr(*orbCorr);
44}
45
46//
47////////////////////////////////////////////////////////////////////////////
48void t_eph::setClkCorr(const t_clkCorr* clkCorr) {
49 if (_clkCorr) {
50 delete _clkCorr;
51 _clkCorr = 0;
52 }
53 _clkCorr = new t_clkCorr(*clkCorr);
54}
55
56//
57////////////////////////////////////////////////////////////////////////////
58t_irc t_eph::getCrd(const bncTime& tt, ColumnVector& xc, ColumnVector& vv, bool useCorr) const {
59
60 if (_checkState == bad ||
61 _checkState == unhealthy ||
62 _checkState == outdated) {
63 return failure;
64 }
65
66 xc.ReSize(6);
67 vv.ReSize(3);
68 if (position(tt.gpsw(), tt.gpssec(), xc.data(), vv.data()) != success) {
69 return failure;
70 }
71 if (useCorr) {
72 if (_orbCorr && _clkCorr) {
73 double dtO = tt - _orbCorr->_time;
74 if (_orbCorr->_updateInt) {
75 dtO -= (0.5 * ssrUpdateInt[_orbCorr->_updateInt]);
76 }
77 ColumnVector dx(3);
78 dx[0] = _orbCorr->_xr[0] + _orbCorr->_dotXr[0] * dtO;
79 dx[1] = _orbCorr->_xr[1] + _orbCorr->_dotXr[1] * dtO;
80 dx[2] = _orbCorr->_xr[2] + _orbCorr->_dotXr[2] * dtO;
81
82 RSW_to_XYZ(xc.Rows(1,3), vv.Rows(1,3), dx, dx);
83
84 xc[0] -= dx[0];
85 xc[1] -= dx[1];
86 xc[2] -= dx[2];
87
88 ColumnVector dv(3);
89 RSW_to_XYZ(xc.Rows(1,3), vv.Rows(1,3), _orbCorr->_dotXr, dv);
90
91 vv[0] -= dv[0];
92 vv[1] -= dv[1];
93 vv[2] -= dv[2];
94
95 double dtC = tt - _clkCorr->_time;
96 if (_clkCorr->_updateInt) {
97 dtC -= (0.5 * ssrUpdateInt[_clkCorr->_updateInt]);
98 }
99 xc[3] += _clkCorr->_dClk + _clkCorr->_dotDClk * dtC + _clkCorr->_dotDotDClk * dtC * dtC;
100 }
101 else {
102 return failure;
103 }
104 }
105 return success;
106}
107
108
109//
110//////////////////////////////////////////////////////////////////////////////
111t_irc t_eph::setNavType(QString navTypeStr) {
112 if (navTypeStr == "LNAV") {_navType = t_eph::LNAV;}
113 else if (navTypeStr == "FDMA") {_navType = t_eph::FDMA;}
114 else if (navTypeStr == "FNAV") {_navType = t_eph::FNAV;}
115 else if (navTypeStr == "INAF") {_navType = t_eph::INAF;}
116 else if (navTypeStr == "D1") {_navType = t_eph::D1;}
117 else if (navTypeStr == "D2") {_navType = t_eph::D2;}
118 else if (navTypeStr == "SBAS") {_navType = t_eph::SBASL1;}
119 else if (navTypeStr == "CNAV") {_navType = t_eph::CNAV;}
120 else if (navTypeStr == "CNV1") {_navType = t_eph::CNV1;}
121 else if (navTypeStr == "CNV2") {_navType = t_eph::CNV2;}
122 else if (navTypeStr == "CNV3") {_navType = t_eph::CNV3;}
123 else {_navType = t_eph::undefined; return failure;}
124
125 return success;
126}
127
128//
129//////////////////////////////////////////////////////////////////////////////
130QString t_eph::navTypeString(e_navType navType, const t_prn& prn, double version) {
131 QString navTypeString = "";
132 QString epochStart;
133 QString eolStr;
134
135 if (version < 4.0) {
136 return navTypeString;
137 }
138
139 if (version == 99.0) {
140 epochStart = "";
141 eolStr = "";
142 }
143 else {
144 epochStart = "> ";
145 eolStr = "\n";
146 }
147
148 QString ephStr = QString("EPH %1 ").arg(prn.toString().c_str());
149 switch (navType) {
150 case undefined:
151 navTypeString = epochStart + ephStr + "unknown" + eolStr;
152 break;
153 case LNAV:
154 navTypeString = epochStart + ephStr + "LNAV" + eolStr;
155 break;
156 case FDMA:
157 navTypeString = epochStart + ephStr + "FDMA" + eolStr;
158 break;
159 case FNAV:
160 navTypeString = epochStart + ephStr + "FNAV" + eolStr;
161 break;
162 case INAF:
163 navTypeString = epochStart + ephStr + "INAV" + eolStr;
164 break;
165 case D1:
166 navTypeString = epochStart + ephStr + "D1 " + eolStr;
167 break;
168 case D2:
169 navTypeString = epochStart + ephStr + "D2 " + eolStr;
170 break;
171 case SBASL1:
172 navTypeString = epochStart + ephStr + "SBAS" + eolStr;
173 break;
174 case CNAV:
175 navTypeString = epochStart + ephStr + "CNAV" + eolStr;
176 break;
177 case CNV1:
178 navTypeString = epochStart + ephStr + "CNV1" + eolStr;
179 break;
180 case CNV2:
181 navTypeString = epochStart + ephStr + "CNV2" + eolStr;
182 break;
183 case CNV3:
184 navTypeString = epochStart + ephStr + "CNV3" + eolStr;
185 break;
186 }
187 return navTypeString;
188 }
189
190//
191//////////////////////////////////////////////////////////////////////////////
192QString t_eph::rinexDateStr(const bncTime& tt, const t_prn& prn, double version) {
193 QString prnStr(prn.toString().c_str());
194 return rinexDateStr(tt, prnStr, version);
195}
196
197//
198//////////////////////////////////////////////////////////////////////////////
199QString t_eph::rinexDateStr(const bncTime& tt, const QString& prnStr, double version) {
200
201 QString datStr;
202
203 unsigned year, month, day, hour, min;
204 double sec;
205 tt.civil_date(year, month, day);
206 tt.civil_time(hour, min, sec);
207
208 QTextStream out(&datStr);
209
210 if (version < 3.0) {
211 QString prnHlp = prnStr.mid(1,2); if (prnHlp[0] == '0') prnHlp[0] = ' ';
212 out << prnHlp << QString(" %1 %2 %3 %4 %5%6")
213 .arg(year % 100, 2, 10, QChar('0'))
214 .arg(month, 2)
215 .arg(day, 2)
216 .arg(hour, 2)
217 .arg(min, 2)
218 .arg(sec, 5, 'f',1);
219 }
220 else if (version == 99) {
221 out << QString(" %1 %2 %3 %4 %5 %6")
222 .arg(year, 4)
223 .arg(month, 2, 10, QChar('0'))
224 .arg(day, 2, 10, QChar('0'))
225 .arg(hour, 2, 10, QChar('0'))
226 .arg(min, 2, 10, QChar('0'))
227 .arg(int(sec), 2, 10, QChar('0'));
228 }
229 else {
230 out << prnStr << QString(" %1 %2 %3 %4 %5 %6")
231 .arg(year, 4)
232 .arg(month, 2, 10, QChar('0'))
233 .arg(day, 2, 10, QChar('0'))
234 .arg(hour, 2, 10, QChar('0'))
235 .arg(min, 2, 10, QChar('0'))
236 .arg(int(sec), 2, 10, QChar('0'));
237 }
238
239 return datStr;
240}
241
242// Constructor
243//////////////////////////////////////////////////////////////////////////////
244t_ephGPS::t_ephGPS(double rnxVersion, const QStringList& lines) {
245
246 const int nLines = 8;
247
248 if (lines.size() != nLines) {
249 _checkState = bad;
250 return;
251 }
252
253 // RINEX Format
254 // ------------
255 int fieldLen = 19;
256
257 int pos[4];
258 pos[0] = (rnxVersion <= 2.12) ? 3 : 4;
259 pos[1] = pos[0] + fieldLen;
260 pos[2] = pos[1] + fieldLen;
261 pos[3] = pos[2] + fieldLen;
262
263 // Read eight lines
264 // ----------------
265 for (int iLine = 0; iLine < nLines; iLine++) {
266 QString line = lines[iLine];
267
268 if ( iLine == 0 ) {
269 QTextStream in(line.left(pos[1]).toLatin1());
270 int year, month, day, hour, min;
271 double sec;
272
273 QString prnStr, n;
274 in >> prnStr;
275
276 if (prnStr.size() == 1 &&
277 (prnStr[0] == 'G' ||
278 prnStr[0] == 'J' ||
279 prnStr[0] == 'I')) {
280 in >> n;
281 prnStr.append(n);
282 }
283
284 in >> year >> month >> day >> hour >> min >> sec;
285 if (prnStr.at(0) == 'G') {
286 _prn.set('G', prnStr.mid(1).toInt());
287 }
288 else if (prnStr.at(0) == 'J') {
289 _prn.set('J', prnStr.mid(1).toInt());
290 }
291 else if (prnStr.at(0) == 'I') {
292 _prn.set('I', prnStr.mid(1).toInt());
293 }
294 else {
295 _prn.set('G', prnStr.toInt());
296 }
297
298 if (year < 80) {
299 year += 2000;
300 }
301 else if (year < 100) {
302 year += 1900;
303 }
304
305 _TOC.set(year, month, day, hour, min, sec);
306
307 if ( readDbl(line, pos[1], fieldLen, _clock_bias ) ||
308 readDbl(line, pos[2], fieldLen, _clock_drift ) ||
309 readDbl(line, pos[3], fieldLen, _clock_driftrate) ) {
310 _checkState = bad;
311 return;
312 }
313 }
314
315 else if ( iLine == 1 ) {
316 if ( readDbl(line, pos[0], fieldLen, _IODE ) ||
317 readDbl(line, pos[1], fieldLen, _Crs ) ||
318 readDbl(line, pos[2], fieldLen, _Delta_n) ||
319 readDbl(line, pos[3], fieldLen, _M0 ) ) {
320 _checkState = bad;
321 return;
322 }
323 }
324
325 else if ( iLine == 2 ) {
326 if ( readDbl(line, pos[0], fieldLen, _Cuc ) ||
327 readDbl(line, pos[1], fieldLen, _e ) ||
328 readDbl(line, pos[2], fieldLen, _Cus ) ||
329 readDbl(line, pos[3], fieldLen, _sqrt_A) ) {
330 _checkState = bad;
331 return;
332 }
333 }
334
335 else if ( iLine == 3 ) {
336 if ( readDbl(line, pos[0], fieldLen, _TOEsec) ||
337 readDbl(line, pos[1], fieldLen, _Cic ) ||
338 readDbl(line, pos[2], fieldLen, _OMEGA0) ||
339 readDbl(line, pos[3], fieldLen, _Cis ) ) {
340 _checkState = bad;
341 return;
342 }
343 }
344
345 else if ( iLine == 4 ) {
346 if ( readDbl(line, pos[0], fieldLen, _i0 ) ||
347 readDbl(line, pos[1], fieldLen, _Crc ) ||
348 readDbl(line, pos[2], fieldLen, _omega ) ||
349 readDbl(line, pos[3], fieldLen, _OMEGADOT) ) {
350 _checkState = bad;
351 return;
352 }
353 }
354
355 else if ( iLine == 5 && type() != t_eph::IRNSS) {
356 if ( readDbl(line, pos[0], fieldLen, _IDOT ) ||
357 readDbl(line, pos[1], fieldLen, _L2Codes) ||
358 readDbl(line, pos[2], fieldLen, _TOEweek ) ||
359 readDbl(line, pos[3], fieldLen, _L2PFlag) ) {
360 _checkState = bad;
361 return;
362 }
363 }
364 else if ( iLine == 5 && type() == t_eph::IRNSS) {
365 if ( readDbl(line, pos[0], fieldLen, _IDOT ) ||
366 readDbl(line, pos[2], fieldLen, _TOEweek) ) {
367 _checkState = bad;
368 return;
369 }
370 }
371
372 else if ( iLine == 6 && type() != t_eph::IRNSS) {
373 if ( readDbl(line, pos[0], fieldLen, _ura ) ||
374 readDbl(line, pos[1], fieldLen, _health) ||
375 readDbl(line, pos[2], fieldLen, _TGD ) ||
376 readDbl(line, pos[3], fieldLen, _IODC ) ) {
377 _checkState = bad;
378 return;
379 }
380 }
381 else if ( iLine == 6 && type() == t_eph::IRNSS) {
382 if ( readDbl(line, pos[0], fieldLen, _ura ) ||
383 readDbl(line, pos[1], fieldLen, _health) ||
384 readDbl(line, pos[2], fieldLen, _TGD ) ) {
385 _checkState = bad;
386 return;
387 }
388 }
389 else if ( iLine == 7 ) {
390 if ( readDbl(line, pos[0], fieldLen, _TOT) ) {
391 _checkState = bad;
392 return;
393 }
394 // fitInterval is not valid for IRNSS
395 if (type() != t_eph::IRNSS) {
396 double fitIntervalRnx;
397 readDbl(line, pos[1], fieldLen, fitIntervalRnx);
398 if (type() == t_eph::GPS) { // in RINEX specified allways as time period for GPS
399 _fitInterval = fitIntervalRnx;
400 } else if (type() == t_eph::QZSS) { // specified as flag for QZSS
401 if (rnxVersion == 3.02) {
402 _fitInterval = fitIntervalRnx; // specified as time period
403 }
404 else {
405 _fitInterval = fitIntervalFromFlag(fitIntervalRnx, _IODC, t_eph::QZSS);
406 }
407 }
408 }
409 }
410 }
411}
412
413// Compute GPS Satellite Position (virtual)
414////////////////////////////////////////////////////////////////////////////
415t_irc t_ephGPS::position(int GPSweek, double GPSweeks, double* xc, double* vv) const {
416
417 static const double omegaEarth = 7292115.1467e-11;
418 static const double gmGRS = 398.6005e12;
419
420 memset(xc, 0, 6*sizeof(double));
421 memset(vv, 0, 3*sizeof(double));
422
423 double a0 = _sqrt_A * _sqrt_A;
424 if (a0 == 0) {
425 return failure;
426 }
427
428 double n0 = sqrt(gmGRS/(a0*a0*a0));
429
430 bncTime tt(GPSweek, GPSweeks);
431 double tk = tt - bncTime(int(_TOEweek), _TOEsec);
432
433 double n = n0 + _Delta_n;
434 double M = _M0 + n*tk;
435 double E = M;
436 double E_last;
437 int nLoop = 0;
438 do {
439 E_last = E;
440 E = M + _e*sin(E);
441
442 if (++nLoop == 100) {
443 return failure;
444 }
445 } while ( fabs(E-E_last)*a0 > 0.001);
446 double v = 2.0*atan( sqrt( (1.0 + _e)/(1.0 - _e) )*tan( E/2 ) );
447 double u0 = v + _omega;
448 double sin2u0 = sin(2*u0);
449 double cos2u0 = cos(2*u0);
450 double r = a0*(1 - _e*cos(E)) + _Crc*cos2u0 + _Crs*sin2u0;
451 double i = _i0 + _IDOT*tk + _Cic*cos2u0 + _Cis*sin2u0;
452 double u = u0 + _Cuc*cos2u0 + _Cus*sin2u0;
453 double xp = r*cos(u);
454 double yp = r*sin(u);
455 double OM = _OMEGA0 + (_OMEGADOT - omegaEarth)*tk -
456 omegaEarth*_TOEsec;
457
458 double sinom = sin(OM);
459 double cosom = cos(OM);
460 double sini = sin(i);
461 double cosi = cos(i);
462 xc[0] = xp*cosom - yp*cosi*sinom;
463 xc[1] = xp*sinom + yp*cosi*cosom;
464 xc[2] = yp*sini;
465
466 double tc = tt - _TOC;
467 xc[3] = _clock_bias + _clock_drift*tc + _clock_driftrate*tc*tc;
468
469 // Velocity
470 // --------
471 double tanv2 = tan(v/2);
472 double dEdM = 1 / (1 - _e*cos(E));
473 double dotv = sqrt((1.0 + _e)/(1.0 - _e)) / cos(E/2)/cos(E/2) / (1 + tanv2*tanv2)
474 * dEdM * n;
475 double dotu = dotv + (-_Cuc*sin2u0 + _Cus*cos2u0)*2*dotv;
476 double dotom = _OMEGADOT - omegaEarth;
477 double doti = _IDOT + (-_Cic*sin2u0 + _Cis*cos2u0)*2*dotv;
478 double dotr = a0 * _e*sin(E) * dEdM * n
479 + (-_Crc*sin2u0 + _Crs*cos2u0)*2*dotv;
480 double dotx = dotr*cos(u) - r*sin(u)*dotu;
481 double doty = dotr*sin(u) + r*cos(u)*dotu;
482
483 vv[0] = cosom *dotx - cosi*sinom *doty // dX / dr
484 - xp*sinom*dotom - yp*cosi*cosom*dotom // dX / dOMEGA
485 + yp*sini*sinom*doti; // dX / di
486
487 vv[1] = sinom *dotx + cosi*cosom *doty
488 + xp*cosom*dotom - yp*cosi*sinom*dotom
489 - yp*sini*cosom*doti;
490
491 vv[2] = sini *doty + yp*cosi *doti;
492
493 // Relativistic Correction
494 // -----------------------
495 xc[3] -= 4.442807633e-10 * _e * sqrt(a0) *sin(E);
496
497 xc[4] = _clock_drift + _clock_driftrate*tc;
498 xc[5] = _clock_driftrate;
499
500 return success;
501}
502
503// RINEX Format String
504//////////////////////////////////////////////////////////////////////////////
505QString t_ephGPS::toString(double version) const {
506
507 QString navStr = navTypeString(_navType, _prn, version);
508 QString rnxStr = navStr + rinexDateStr(_TOC, _prn, version);
509
510 QTextStream out(&rnxStr);
511
512 out << QString("%1%2%3\n")
513 .arg(_clock_bias, 19, 'e', 12)
514 .arg(_clock_drift, 19, 'e', 12)
515 .arg(_clock_driftrate, 19, 'e', 12);
516
517 QString fmt = version < 3.0 ? " %1%2%3%4\n" : " %1%2%3%4\n";
518
519 out << QString(fmt)
520 .arg(_IODE, 19, 'e', 12)
521 .arg(_Crs, 19, 'e', 12)
522 .arg(_Delta_n, 19, 'e', 12)
523 .arg(_M0, 19, 'e', 12);
524
525 out << QString(fmt)
526 .arg(_Cuc, 19, 'e', 12)
527 .arg(_e, 19, 'e', 12)
528 .arg(_Cus, 19, 'e', 12)
529 .arg(_sqrt_A, 19, 'e', 12);
530
531 out << QString(fmt)
532 .arg(_TOEsec, 19, 'e', 12)
533 .arg(_Cic, 19, 'e', 12)
534 .arg(_OMEGA0, 19, 'e', 12)
535 .arg(_Cis, 19, 'e', 12);
536
537 out << QString(fmt)
538 .arg(_i0, 19, 'e', 12)
539 .arg(_Crc, 19, 'e', 12)
540 .arg(_omega, 19, 'e', 12)
541 .arg(_OMEGADOT, 19, 'e', 12);
542
543 if (type() == t_eph::IRNSS) {
544 out << QString(fmt)
545 .arg(_IDOT, 19, 'e', 12)
546 .arg(0.0, 19, 'e', 12)
547 .arg(_TOEweek, 19, 'e', 12)
548 .arg(0.0, 19, 'e', 12);
549 }
550 else {
551 out << QString(fmt)
552 .arg(_IDOT, 19, 'e', 12)
553 .arg(_L2Codes, 19, 'e', 12)
554 .arg(_TOEweek, 19, 'e', 12)
555 .arg(_L2PFlag, 19, 'e', 12);
556 }
557
558 if (type() == t_eph::IRNSS) {
559 out << QString(fmt)
560 .arg(_ura, 19, 'e', 12)
561 .arg(_health, 19, 'e', 12)
562 .arg(_TGD, 19, 'e', 12)
563 .arg(0.0, 19, 'e', 12);
564 }
565 else {
566 out << QString(fmt)
567 .arg(_ura, 19, 'e', 12)
568 .arg(_health, 19, 'e', 12)
569 .arg(_TGD, 19, 'e', 12)
570 .arg(_IODC, 19, 'e', 12);
571 }
572
573 double tot = _TOT;
574 if (tot == 0.9999e9 && version < 3.0) {
575 tot = 0.0;
576 }
577 // fitInterval
578 if (type() == t_eph::IRNSS) {// not valid for IRNSS
579 out << QString(fmt)
580 .arg(tot, 19, 'e', 12)
581 .arg(0.0, 19, 'e', 12)
582 .arg("", 19, QChar(' '))
583 .arg("", 19, QChar(' '));
584 }
585 else {
586 // for GPS and QZSS in version 3.02 specified in hours
587 double fitIntervalRnx = _fitInterval;
588 // otherwise specified as flag
589 if (type() == t_eph::QZSS && version != 3.02) {
590 (_fitInterval == 2.0) ? fitIntervalRnx = 0.0 : fitIntervalRnx = 1.0;
591 }
592 out << QString(fmt)
593 .arg(tot, 19, 'e', 12)
594 .arg(fitIntervalRnx, 19, 'e', 12)
595 .arg("", 19, QChar(' '))
596 .arg("", 19, QChar(' '));
597 }
598 return rnxStr;
599}
600
601// Constructor
602//////////////////////////////////////////////////////////////////////////////
603t_ephGlo::t_ephGlo(double rnxVersion, const QStringList& lines) {
604
605 int nLines = 4;
606 if (rnxVersion >= 3.05) {
607 nLines += 1;
608 _flags_unknown = false;
609 }
610 else {
611 _M_delta_tau = 0.9999e9; // unknown
612 _M_FT = 1.5e1; // unknown
613 _flags_unknown = true;
614 }
615
616 if (lines.size() != nLines) {
617 _checkState = bad;
618 return;
619 }
620
621 // RINEX Format
622 // ------------
623 int fieldLen = 19;
624 double statusflags = 0.0;
625 double healthflags = 0.0;
626
627 int pos[4];
628 pos[0] = (rnxVersion <= 2.12) ? 3 : 4;
629 pos[1] = pos[0] + fieldLen;
630 pos[2] = pos[1] + fieldLen;
631 pos[3] = pos[2] + fieldLen;
632
633 // Read four lines
634 // ---------------
635 for (int iLine = 0; iLine < nLines; iLine++) {
636 QString line = lines[iLine];
637
638 if ( iLine == 0 ) {
639 QTextStream in(line.left(pos[1]).toLatin1());
640
641 int year, month, day, hour, min;
642 double sec;
643
644 QString prnStr, n;
645 in >> prnStr;
646 if (prnStr.size() == 1 && prnStr[0] == 'R') {
647 in >> n;
648 prnStr.append(n);
649 }
650 in >> year >> month >> day >> hour >> min >> sec;
651 if (prnStr.at(0) == 'R') {
652 _prn.set('R', prnStr.mid(1).toInt());
653 }
654 else {
655 _prn.set('R', prnStr.toInt());
656 }
657
658 if (year < 80) {
659 year += 2000;
660 }
661 else if (year < 100) {
662 year += 1900;
663 }
664
665 _gps_utc = gnumleap(year, month, day);
666
667 _TOC.set(year, month, day, hour, min, sec);
668 _TOC = _TOC + _gps_utc;
669 int nd = int((_TOC.gpssec())) / (24.0*60.0*60.0);
670 if ( readDbl(line, pos[1], fieldLen, _tau ) ||
671 readDbl(line, pos[2], fieldLen, _gamma) ||
672 readDbl(line, pos[3], fieldLen, _tki ) ) {
673 _checkState = bad;
674 return;
675 }
676 _tki -= nd * 86400.0;
677 _tau = -_tau;
678 }
679
680 else if ( iLine == 1 ) {
681 if ( readDbl(line, pos[0], fieldLen, _x_pos ) ||
682 readDbl(line, pos[1], fieldLen, _x_velocity ) ||
683 readDbl(line, pos[2], fieldLen, _x_acceleration) ||
684 readDbl(line, pos[3], fieldLen, _health ) ) {
685 _checkState = bad;
686 return;
687 }
688 }
689
690 else if ( iLine == 2 ) {
691 if ( readDbl(line, pos[0], fieldLen, _y_pos ) ||
692 readDbl(line, pos[1], fieldLen, _y_velocity ) ||
693 readDbl(line, pos[2], fieldLen, _y_acceleration ) ||
694 readDbl(line, pos[3], fieldLen, _frequency_number) ) {
695 _checkState = bad;
696 return;
697 }
698 }
699
700 else if ( iLine == 3 ) {
701 if ( readDbl(line, pos[0], fieldLen, _z_pos ) ||
702 readDbl(line, pos[1], fieldLen, _z_velocity ) ||
703 readDbl(line, pos[2], fieldLen, _z_acceleration) ||
704 readDbl(line, pos[3], fieldLen, _E ) ) {
705 _checkState = bad;
706 return;
707 }
708 }
709
710 else if ( iLine == 4 ) {
711 if ( readDbl(line, pos[0], fieldLen, statusflags ) ||
712 readDbl(line, pos[1], fieldLen, _M_delta_tau ) ||
713 readDbl(line, pos[2], fieldLen, _M_FT ) ||
714 readDbl(line, pos[3], fieldLen, healthflags ) ) {
715 _checkState = bad;
716 return;
717 }
718 else {
719 // status flags
720 // ============
721 // bit 0-1
722 _M_P = double(bitExtracted(statusflags, 2, 0));
723 // bit 2-3
724 _P1 = double(bitExtracted(statusflags, 2, 2));
725 // bit 4
726 _P2 = double(bitExtracted(statusflags, 1, 4));
727 // bit 5
728 _P3 = double(bitExtracted(statusflags, 1, 5));
729 // bit 6
730 _M_P4 = double(bitExtracted(statusflags, 1, 6));
731 // bit 7-8
732 _M_M = double(bitExtracted(statusflags, 2, 7));
733 /// GLO M/K exclusive flags/values only valid if flag M is set to '01'
734 if (!_M_M) {
735 _M_P4 = 0.0;
736 _M_P = 0.0;
737 }
738 // health flags
739 // ============
740 // bit 0 (is to be ignored, if bit 1 is zero)
741 _almanac_health = double(bitExtracted(healthflags, 1, 0));
742 // bit 1
743 _almanac_health_availablility_indicator = double(bitExtracted(healthflags, 1, 1));
744 // bit 2
745 _M_l3 = double(bitExtracted(healthflags, 1, 2));
746 }
747 }
748 }
749
750 // Initialize status vector
751 // ------------------------
752 _tt = _TOC;
753 _xv.ReSize(6); _xv = 0.0;
754 _xv(1) = _x_pos * 1.e3;
755 _xv(2) = _y_pos * 1.e3;
756 _xv(3) = _z_pos * 1.e3;
757 _xv(4) = _x_velocity * 1.e3;
758 _xv(5) = _y_velocity * 1.e3;
759 _xv(6) = _z_velocity * 1.e3;
760}
761
762// Compute Glonass Satellite Position (virtual)
763////////////////////////////////////////////////////////////////////////////
764t_irc t_ephGlo::position(int GPSweek, double GPSweeks, double* xc, double* vv) const {
765
766 static const double nominalStep = 10.0;
767
768 memset(xc, 0, 6*sizeof(double));
769 memset(vv, 0, 3*sizeof(double));
770
771 double dtPos = bncTime(GPSweek, GPSweeks) - _tt;
772
773 if (fabs(dtPos) > 24 * 3600.0) {
774 return failure;
775 }
776
777 int nSteps = int(fabs(dtPos) / nominalStep) + 1;
778 double step = dtPos / nSteps;
779
780 double acc[3];
781 acc[0] = _x_acceleration * 1.e3;
782 acc[1] = _y_acceleration * 1.e3;
783 acc[2] = _z_acceleration * 1.e3;
784
785 for (int ii = 1; ii <= nSteps; ii++) {
786 _xv = rungeKutta4(_tt.gpssec(), _xv, step, acc, glo_deriv);
787 _tt = _tt + step;
788 }
789
790 // Position and Velocity
791 // ---------------------
792 xc[0] = _xv(1);
793 xc[1] = _xv(2);
794 xc[2] = _xv(3);
795
796 vv[0] = _xv(4);
797 vv[1] = _xv(5);
798 vv[2] = _xv(6);
799
800 // Clock Correction
801 // ----------------
802 double dtClk = bncTime(GPSweek, GPSweeks) - _TOC;
803 xc[3] = -_tau + _gamma * dtClk;
804
805 xc[4] = _gamma;
806 xc[5] = 0.0;
807
808 return success;
809}
810
811// RINEX Format String
812//////////////////////////////////////////////////////////////////////////////
813QString t_ephGlo::toString(double version) const {
814
815 QString navStr = navTypeString(_navType, _prn, version);
816 QString rnxStr = navStr + rinexDateStr(_TOC -_gps_utc, _prn, version);
817 int nd = int((_TOC - _gps_utc).gpssec()) / (24.0*60.0*60.0);
818 QTextStream out(&rnxStr);
819
820 out << QString("%1%2%3\n")
821 .arg(-_tau, 19, 'e', 12)
822 .arg(_gamma, 19, 'e', 12)
823 .arg(_tki+nd*86400.0, 19, 'e', 12);
824
825 QString fmt = version < 3.0 ? " %1%2%3%4\n" : " %1%2%3%4\n";
826
827 out << QString(fmt)
828 .arg(_x_pos, 19, 'e', 12)
829 .arg(_x_velocity, 19, 'e', 12)
830 .arg(_x_acceleration, 19, 'e', 12)
831 .arg(_health, 19, 'e', 12);
832
833 out << QString(fmt)
834 .arg(_y_pos, 19, 'e', 12)
835 .arg(_y_velocity, 19, 'e', 12)
836 .arg(_y_acceleration, 19, 'e', 12)
837 .arg(_frequency_number, 19, 'e', 12);
838
839 out << QString(fmt)
840 .arg(_z_pos, 19, 'e', 12)
841 .arg(_z_velocity, 19, 'e', 12)
842 .arg(_z_acceleration, 19, 'e', 12)
843 .arg(_E, 19, 'e', 12);
844
845 if (version >= 3.05) {
846 // unknown (RINEX version < 3.05)
847 if (_flags_unknown) {
848 out << QString(fmt)
849 .arg("", 19, QChar(' ')) // statusflags blank if unknown
850 .arg(_M_delta_tau, 19, 'e', 12)
851 .arg(_M_FT, 19, 'e', 12)
852 .arg("", 19, QChar(' ')); // healthflags blank if unknown
853 }
854 else {
855 int statusflags = 0;
856 // bit 7-8
857 if (_M_M == 2.0) {
858 statusflags |= (1<<7);
859 }
860 // bit 6
861 if (_M_P4) {
862 statusflags |= (1<<6);
863 }
864 // bit 5
865 if (_P3) {
866 statusflags |= (1<<5);
867 }
868 // bit 4
869 if (_P2) {
870 statusflags |= (1<<4);
871 }
872 // bit 2-3
873 if (_P1 == 2.0) {
874 statusflags |= (1<<2);
875 }
876 else if (_P1 == 1.0) {
877 statusflags |= (1<<3);
878 }
879 else if (_P1 == 3.0) {
880 statusflags |= (1<<2);
881 statusflags |= (1<<3);
882 }
883 // bit 0-1
884 if (_M_P == 2.0) {
885 statusflags |= (1<<0);
886 }
887 else if (_M_P == 1.0) {
888 statusflags |= (1<<1);
889 }
890 else if (_M_P == 3.0) {
891 statusflags |= (1<<0);
892 statusflags |= (1<<1);
893 }
894 // health flags
895 // ============
896 int healthflags = 0;
897 // bit 0 (is to be ignored, if bit 1 is zero)
898 if (_almanac_health) {
899 healthflags |= (1<<0);
900 }
901 // bit 1
902 if (_almanac_health_availablility_indicator) {
903 healthflags |= (1<<1);
904 }
905 // bit 2
906 if (_M_l3) {
907 healthflags |= (1<<2);
908 }
909 out << QString(fmt)
910 .arg(double(statusflags), 19, 'e', 12)
911 .arg(_M_delta_tau, 19, 'e', 12)
912 .arg(_M_FT, 19, 'e', 12)
913 .arg(double(healthflags), 19, 'e', 12);
914 }
915 }
916
917 return rnxStr;
918}
919
920// Derivative of the state vector using a simple force model (static)
921////////////////////////////////////////////////////////////////////////////
922ColumnVector t_ephGlo::glo_deriv(double /* tt */, const ColumnVector& xv,
923 double* acc) {
924
925 // State vector components
926 // -----------------------
927 ColumnVector rr = xv.rows(1,3);
928 ColumnVector vv = xv.rows(4,6);
929
930 // Acceleration
931 // ------------
932 static const double gmWGS = 398.60044e12;
933 static const double AE = 6378136.0;
934 static const double OMEGA = 7292115.e-11;
935 static const double C20 = -1082.6257e-6;
936
937 double rho = rr.NormFrobenius();
938 double t1 = -gmWGS/(rho*rho*rho);
939 double t2 = 3.0/2.0 * C20 * (gmWGS*AE*AE) / (rho*rho*rho*rho*rho);
940 double t3 = OMEGA * OMEGA;
941 double t4 = 2.0 * OMEGA;
942 double z2 = rr(3) * rr(3);
943
944 // Vector of derivatives
945 // ---------------------
946 ColumnVector va(6);
947 va(1) = vv(1);
948 va(2) = vv(2);
949 va(3) = vv(3);
950 va(4) = (t1 + t2*(1.0-5.0*z2/(rho*rho)) + t3) * rr(1) + t4*vv(2) + acc[0];
951 va(5) = (t1 + t2*(1.0-5.0*z2/(rho*rho)) + t3) * rr(2) - t4*vv(1) + acc[1];
952 va(6) = (t1 + t2*(3.0-5.0*z2/(rho*rho)) ) * rr(3) + acc[2];
953
954 return va;
955}
956
957// IOD of Glonass Ephemeris (virtual)
958////////////////////////////////////////////////////////////////////////////
959unsigned int t_ephGlo::IOD() const {
960 bncTime tMoscow = _TOC - _gps_utc + 3 * 3600.0;
961 return (unsigned long)tMoscow.daysec() / 900;
962}
963
964// Health status of Glonass Ephemeris (virtual)
965////////////////////////////////////////////////////////////////////////////
966unsigned int t_ephGlo::isUnhealthy() const {
967
968 if (_almanac_health_availablility_indicator) {
969 if ((_health == 0 && _almanac_health == 0) ||
970 (_health == 1 && _almanac_health == 0) ||
971 (_health == 1 && _almanac_health == 1)) {
972 return 1;
973 }
974 }
975 else if (!_almanac_health_availablility_indicator) {
976 if (_health) {
977 return 1;
978 }
979 }
980 return 0; /* (_health == 0 && _almanac_health == 1) or (_health == 0) */
981}
982
983// Constructor
984//////////////////////////////////////////////////////////////////////////////
985t_ephGal::t_ephGal(double rnxVersion, const QStringList& lines) {
986 int year, month, day, hour, min;
987 double sec;
988 QString prnStr;
989 const int nLines = 8;
990 if (lines.size() != nLines) {
991 _checkState = bad;
992 return;
993 }
994
995 // RINEX Format
996 // ------------
997 int fieldLen = 19;
998 double SVhealth = 0.0;
999 double datasource = 0.0;
1000
1001 int pos[4];
1002 pos[0] = (rnxVersion <= 2.12) ? 3 : 4;
1003 pos[1] = pos[0] + fieldLen;
1004 pos[2] = pos[1] + fieldLen;
1005 pos[3] = pos[2] + fieldLen;
1006
1007 // Read eight lines
1008 // ----------------
1009 for (int iLine = 0; iLine < nLines; iLine++) {
1010 QString line = lines[iLine];
1011
1012 if ( iLine == 0 ) {
1013 QTextStream in(line.left(pos[1]).toLatin1());
1014 QString n;
1015 in >> prnStr;
1016 if (prnStr.size() == 1 && prnStr[0] == 'E') {
1017 in >> n;
1018 prnStr.append(n);
1019 }
1020 in >> year >> month >> day >> hour >> min >> sec;
1021 if (year < 80) {
1022 year += 2000;
1023 }
1024 else if (year < 100) {
1025 year += 1900;
1026 }
1027
1028 _TOC.set(year, month, day, hour, min, sec);
1029
1030 if ( readDbl(line, pos[1], fieldLen, _clock_bias ) ||
1031 readDbl(line, pos[2], fieldLen, _clock_drift ) ||
1032 readDbl(line, pos[3], fieldLen, _clock_driftrate) ) {
1033 _checkState = bad;
1034 return;
1035 }
1036 }
1037
1038 else if ( iLine == 1 ) {
1039 if ( readDbl(line, pos[0], fieldLen, _IODnav ) ||
1040 readDbl(line, pos[1], fieldLen, _Crs ) ||
1041 readDbl(line, pos[2], fieldLen, _Delta_n) ||
1042 readDbl(line, pos[3], fieldLen, _M0 ) ) {
1043 _checkState = bad;
1044 return;
1045 }
1046 }
1047
1048 else if ( iLine == 2 ) {
1049 if ( readDbl(line, pos[0], fieldLen, _Cuc ) ||
1050 readDbl(line, pos[1], fieldLen, _e ) ||
1051 readDbl(line, pos[2], fieldLen, _Cus ) ||
1052 readDbl(line, pos[3], fieldLen, _sqrt_A) ) {
1053 _checkState = bad;
1054 return;
1055 }
1056 }
1057
1058 else if ( iLine == 3 ) {
1059 if ( readDbl(line, pos[0], fieldLen, _TOEsec) ||
1060 readDbl(line, pos[1], fieldLen, _Cic ) ||
1061 readDbl(line, pos[2], fieldLen, _OMEGA0) ||
1062 readDbl(line, pos[3], fieldLen, _Cis ) ) {
1063 _checkState = bad;
1064 return;
1065 }
1066 }
1067
1068 else if ( iLine == 4 ) {
1069 if ( readDbl(line, pos[0], fieldLen, _i0 ) ||
1070 readDbl(line, pos[1], fieldLen, _Crc ) ||
1071 readDbl(line, pos[2], fieldLen, _omega ) ||
1072 readDbl(line, pos[3], fieldLen, _OMEGADOT) ) {
1073 _checkState = bad;
1074 return;
1075 }
1076 }
1077
1078 else if ( iLine == 5 ) {
1079 if ( readDbl(line, pos[0], fieldLen, _IDOT ) ||
1080 readDbl(line, pos[1], fieldLen, datasource) ||
1081 readDbl(line, pos[2], fieldLen, _TOEweek ) ) {
1082 _checkState = bad;
1083 return;
1084 } else {
1085 if (int(datasource) & (1<<8)) {
1086 _fnav = true;
1087 _inav = false;
1088 } else if (int(datasource) & (1<<9)) {
1089 _fnav = false;
1090 _inav = true;
1091 }
1092 _TOEweek -= 1024.0;
1093 }
1094 }
1095
1096 else if ( iLine == 6 ) {
1097 if ( readDbl(line, pos[0], fieldLen, _SISA ) ||
1098 readDbl(line, pos[1], fieldLen, SVhealth) ||
1099 readDbl(line, pos[2], fieldLen, _BGD_1_5A) ||
1100 readDbl(line, pos[3], fieldLen, _BGD_1_5B) ) {
1101 _checkState = bad;
1102 return;
1103 } else {
1104 // Bit 0
1105 _e1DataInValid = (int(SVhealth) & (1<<0));
1106 // Bit 1-2
1107 _E1_bHS = double((int(SVhealth) >> 1) & 0x3);
1108 // Bit 3
1109 _e5aDataInValid = (int(SVhealth) & (1<<3));
1110 // Bit 4-5
1111 _E5aHS = double((int(SVhealth) >> 4) & 0x3);
1112 // Bit 6
1113 _e5bDataInValid = (int(SVhealth) & (1<<6));
1114 // Bit 7-8
1115 _E5bHS = double((int(SVhealth) >> 7) & 0x3);
1116
1117 if (prnStr.at(0) == 'E') {
1118 _prn.set('E', prnStr.mid(1).toInt(), _inav ? 1 : 0);
1119 }
1120 }
1121 }
1122
1123 else if ( iLine == 7 ) {
1124 if ( readDbl(line, pos[0], fieldLen, _TOT) ) {
1125 _checkState = bad;
1126 return;
1127 }
1128 }
1129 }
1130}
1131
1132// Compute Galileo Satellite Position (virtual)
1133////////////////////////////////////////////////////////////////////////////
1134t_irc t_ephGal::position(int GPSweek, double GPSweeks, double* xc, double* vv) const {
1135
1136 static const double omegaEarth = 7292115.1467e-11;
1137 static const double gmWGS = 398.6004418e12;
1138
1139 memset(xc, 0, 6*sizeof(double));
1140 memset(vv, 0, 3*sizeof(double));
1141
1142 double a0 = _sqrt_A * _sqrt_A;
1143 if (a0 == 0) {
1144 return failure;
1145 }
1146
1147 double n0 = sqrt(gmWGS/(a0*a0*a0));
1148
1149 bncTime tt(GPSweek, GPSweeks);
1150 double tk = tt - bncTime(_TOC.gpsw(), _TOEsec);
1151
1152 double n = n0 + _Delta_n;
1153 double M = _M0 + n*tk;
1154 double E = M;
1155 double E_last;
1156 int nLoop = 0;
1157 do {
1158 E_last = E;
1159 E = M + _e*sin(E);
1160
1161 if (++nLoop == 100) {
1162 return failure;
1163 }
1164 } while ( fabs(E-E_last)*a0 > 0.001 );
1165 double v = 2.0*atan( sqrt( (1.0 + _e)/(1.0 - _e) )*tan( E/2 ) );
1166 double u0 = v + _omega;
1167 double sin2u0 = sin(2*u0);
1168 double cos2u0 = cos(2*u0);
1169 double r = a0*(1 - _e*cos(E)) + _Crc*cos2u0 + _Crs*sin2u0;
1170 double i = _i0 + _IDOT*tk + _Cic*cos2u0 + _Cis*sin2u0;
1171 double u = u0 + _Cuc*cos2u0 + _Cus*sin2u0;
1172 double xp = r*cos(u);
1173 double yp = r*sin(u);
1174 double OM = _OMEGA0 + (_OMEGADOT - omegaEarth)*tk -
1175 omegaEarth*_TOEsec;
1176
1177 double sinom = sin(OM);
1178 double cosom = cos(OM);
1179 double sini = sin(i);
1180 double cosi = cos(i);
1181 xc[0] = xp*cosom - yp*cosi*sinom;
1182 xc[1] = xp*sinom + yp*cosi*cosom;
1183 xc[2] = yp*sini;
1184
1185 double tc = tt - _TOC;
1186 xc[3] = _clock_bias + _clock_drift*tc + _clock_driftrate*tc*tc;
1187
1188 // Velocity
1189 // --------
1190 double tanv2 = tan(v/2);
1191 double dEdM = 1 / (1 - _e*cos(E));
1192 double dotv = sqrt((1.0 + _e)/(1.0 - _e)) / cos(E/2)/cos(E/2) / (1 + tanv2*tanv2)
1193 * dEdM * n;
1194 double dotu = dotv + (-_Cuc*sin2u0 + _Cus*cos2u0)*2*dotv;
1195 double dotom = _OMEGADOT - omegaEarth;
1196 double doti = _IDOT + (-_Cic*sin2u0 + _Cis*cos2u0)*2*dotv;
1197 double dotr = a0 * _e*sin(E) * dEdM * n
1198 + (-_Crc*sin2u0 + _Crs*cos2u0)*2*dotv;
1199 double dotx = dotr*cos(u) - r*sin(u)*dotu;
1200 double doty = dotr*sin(u) + r*cos(u)*dotu;
1201
1202 vv[0] = cosom *dotx - cosi*sinom *doty // dX / dr
1203 - xp*sinom*dotom - yp*cosi*cosom*dotom // dX / dOMEGA
1204 + yp*sini*sinom*doti; // dX / di
1205
1206 vv[1] = sinom *dotx + cosi*cosom *doty
1207 + xp*cosom*dotom - yp*cosi*sinom*dotom
1208 - yp*sini*cosom*doti;
1209
1210 vv[2] = sini *doty + yp*cosi *doti;
1211
1212 // Relativistic Correction
1213 // -----------------------
1214 xc[3] -= 4.442807309e-10 * _e * sqrt(a0) *sin(E);
1215
1216 xc[4] = _clock_drift + _clock_driftrate*tc;
1217 xc[5] = _clock_driftrate;
1218
1219 return success;
1220}
1221
1222// Health status of Galileo Ephemeris (virtual)
1223////////////////////////////////////////////////////////////////////////////
1224unsigned int t_ephGal::isUnhealthy() const {
1225 if (_E5aHS && _E5bHS && _E1_bHS) {
1226 return 1;
1227 }
1228 return 0;
1229}
1230
1231// RINEX Format String
1232//////////////////////////////////////////////////////////////////////////////
1233QString t_ephGal::toString(double version) const {
1234
1235 QString navStr = navTypeString(_navType, _prn, version);
1236 QString rnxStr = navStr + rinexDateStr(_TOC, _prn, version);
1237
1238 QTextStream out(&rnxStr);
1239
1240 out << QString("%1%2%3\n")
1241 .arg(_clock_bias, 19, 'e', 12)
1242 .arg(_clock_drift, 19, 'e', 12)
1243 .arg(_clock_driftrate, 19, 'e', 12);
1244
1245 QString fmt = version < 3.0 ? " %1%2%3%4\n" : " %1%2%3%4\n";
1246
1247 out << QString(fmt)
1248 .arg(_IODnav, 19, 'e', 12)
1249 .arg(_Crs, 19, 'e', 12)
1250 .arg(_Delta_n, 19, 'e', 12)
1251 .arg(_M0, 19, 'e', 12);
1252
1253 out << QString(fmt)
1254 .arg(_Cuc, 19, 'e', 12)
1255 .arg(_e, 19, 'e', 12)
1256 .arg(_Cus, 19, 'e', 12)
1257 .arg(_sqrt_A, 19, 'e', 12);
1258
1259 out << QString(fmt)
1260 .arg(_TOEsec, 19, 'e', 12)
1261 .arg(_Cic, 19, 'e', 12)
1262 .arg(_OMEGA0, 19, 'e', 12)
1263 .arg(_Cis, 19, 'e', 12);
1264
1265 out << QString(fmt)
1266 .arg(_i0, 19, 'e', 12)
1267 .arg(_Crc, 19, 'e', 12)
1268 .arg(_omega, 19, 'e', 12)
1269 .arg(_OMEGADOT, 19, 'e', 12);
1270
1271 int dataSource = 0;
1272 int SVhealth = 0;
1273 double BGD_1_5A = _BGD_1_5A;
1274 double BGD_1_5B = _BGD_1_5B;
1275 if (_fnav) {
1276 dataSource |= (1<<1);
1277 dataSource |= (1<<8);
1278 BGD_1_5B = 0.0;
1279 // SVhealth
1280 // Bit 3 : E5a DVS
1281 if (_e5aDataInValid) {
1282 SVhealth |= (1<<3);
1283 }
1284 // Bit 4-5: E5a HS
1285 if (_E5aHS == 1.0) {
1286 SVhealth |= (1<<4);
1287 }
1288 else if (_E5aHS == 2.0) {
1289 SVhealth |= (1<<5);
1290 }
1291 else if (_E5aHS == 3.0) {
1292 SVhealth |= (1<<4);
1293 SVhealth |= (1<<5);
1294 }
1295 }
1296 else if(_inav) {
1297 // Bit 2 and 0 are set because from MT1046 the data source cannot be determined
1298 // and RNXv3.03 says both can be set if the navigation messages were merged
1299 dataSource |= (1<<0);
1300 dataSource |= (1<<2);
1301 dataSource |= (1<<9);
1302 // SVhealth
1303 // Bit 0 : E1-B DVS
1304 if (_e1DataInValid) {
1305 SVhealth |= (1<<0);
1306 }
1307 // Bit 1-2: E1-B HS
1308 if (_E1_bHS == 1.0) {
1309 SVhealth |= (1<<1);
1310 }
1311 else if (_E1_bHS == 2.0) {
1312 SVhealth |= (1<<2);
1313 }
1314 else if (_E1_bHS == 3.0) {
1315 SVhealth |= (1<<1);
1316 SVhealth |= (1<<2);
1317 }
1318 // Bit 3 : E5a DVS
1319 if (_e5aDataInValid) {
1320 SVhealth |= (1<<3);
1321 }
1322 // Bit 4-5: E5a HS
1323 if (_E5aHS == 1.0) {
1324 SVhealth |= (1<<4);
1325 }
1326 else if (_E5aHS == 2.0) {
1327 SVhealth |= (1<<5);
1328 }
1329 else if (_E5aHS == 3.0) {
1330 SVhealth |= (1<<4);
1331 SVhealth |= (1<<5);
1332 }
1333 // Bit 6 : E5b DVS
1334 if (_e5bDataInValid) {
1335 SVhealth |= (1<<6);
1336 }
1337 // Bit 7-8: E5b HS
1338 if (_E5bHS == 1.0) {
1339 SVhealth |= (1<<7);
1340 }
1341 else if (_E5bHS == 2.0) {
1342 SVhealth |= (1<<8);
1343 }
1344 else if (_E5bHS == 3.0) {
1345 SVhealth |= (1<<7);
1346 SVhealth |= (1<<8);
1347 }
1348 }
1349
1350 out << QString(fmt)
1351 .arg(_IDOT, 19, 'e', 12)
1352 .arg(double(dataSource), 19, 'e', 12)
1353 .arg(_TOEweek + 1024.0, 19, 'e', 12)
1354 .arg(0.0, 19, 'e', 12);
1355
1356 out << QString(fmt)
1357 .arg(_SISA, 19, 'e', 12)
1358 .arg(double(SVhealth), 19, 'e', 12)
1359 .arg(BGD_1_5A, 19, 'e', 12)
1360 .arg(BGD_1_5B, 19, 'e', 12);
1361
1362 double tot = _TOT;
1363 if (tot == 0.9999e9 && version < 3.0) {
1364 tot = 0.0;
1365 }
1366 out << QString(fmt)
1367 .arg(tot, 19, 'e', 12)
1368 .arg("", 19, QChar(' '))
1369 .arg("", 19, QChar(' '))
1370 .arg("", 19, QChar(' '));
1371
1372 return rnxStr;
1373}
1374
1375// Constructor
1376//////////////////////////////////////////////////////////////////////////////
1377t_ephSBAS::t_ephSBAS(double rnxVersion, const QStringList& lines) {
1378
1379 const int nLines = 4;
1380
1381 if (lines.size() != nLines) {
1382 _checkState = bad;
1383 return;
1384 }
1385
1386 // RINEX Format
1387 // ------------
1388 int fieldLen = 19;
1389
1390 int pos[4];
1391 pos[0] = (rnxVersion <= 2.12) ? 3 : 4;
1392 pos[1] = pos[0] + fieldLen;
1393 pos[2] = pos[1] + fieldLen;
1394 pos[3] = pos[2] + fieldLen;
1395
1396 // Read four lines
1397 // ---------------
1398 for (int iLine = 0; iLine < nLines; iLine++) {
1399 QString line = lines[iLine];
1400
1401 if ( iLine == 0 ) {
1402 QTextStream in(line.left(pos[1]).toLatin1());
1403
1404 int year, month, day, hour, min;
1405 double sec;
1406
1407 QString prnStr, n;
1408 in >> prnStr;
1409 if (prnStr.size() == 1 && prnStr[0] == 'S') {
1410 in >> n;
1411 prnStr.append(n);
1412 }
1413 in >> year >> month >> day >> hour >> min >> sec;
1414 if (prnStr.at(0) == 'S') {
1415 _prn.set('S', prnStr.mid(1).toInt());
1416 }
1417 else {
1418 _prn.set('S', prnStr.toInt());
1419 }
1420
1421 if (year < 80) {
1422 year += 2000;
1423 }
1424 else if (year < 100) {
1425 year += 1900;
1426 }
1427
1428 _TOC.set(year, month, day, hour, min, sec);
1429
1430 if ( readDbl(line, pos[1], fieldLen, _agf0 ) ||
1431 readDbl(line, pos[2], fieldLen, _agf1 ) ||
1432 readDbl(line, pos[3], fieldLen, _TOT ) ) {
1433 _checkState = bad;
1434 return;
1435 }
1436 }
1437
1438 else if ( iLine == 1 ) {
1439 if ( readDbl(line, pos[0], fieldLen, _x_pos ) ||
1440 readDbl(line, pos[1], fieldLen, _x_velocity ) ||
1441 readDbl(line, pos[2], fieldLen, _x_acceleration) ||
1442 readDbl(line, pos[3], fieldLen, _health ) ) {
1443 _checkState = bad;
1444 return;
1445 }
1446 }
1447
1448 else if ( iLine == 2 ) {
1449 if ( readDbl(line, pos[0], fieldLen, _y_pos ) ||
1450 readDbl(line, pos[1], fieldLen, _y_velocity ) ||
1451 readDbl(line, pos[2], fieldLen, _y_acceleration ) ||
1452 readDbl(line, pos[3], fieldLen, _ura ) ) {
1453 _checkState = bad;
1454 return;
1455 }
1456 }
1457
1458 else if ( iLine == 3 ) {
1459 double iodn;
1460 if ( readDbl(line, pos[0], fieldLen, _z_pos ) ||
1461 readDbl(line, pos[1], fieldLen, _z_velocity ) ||
1462 readDbl(line, pos[2], fieldLen, _z_acceleration) ||
1463 readDbl(line, pos[3], fieldLen, iodn ) ) {
1464 _checkState = bad;
1465 return;
1466 } else {
1467 _IODN = int(iodn);
1468 }
1469 }
1470 }
1471
1472 _x_pos *= 1.e3;
1473 _y_pos *= 1.e3;
1474 _z_pos *= 1.e3;
1475 _x_velocity *= 1.e3;
1476 _y_velocity *= 1.e3;
1477 _z_velocity *= 1.e3;
1478 _x_acceleration *= 1.e3;
1479 _y_acceleration *= 1.e3;
1480 _z_acceleration *= 1.e3;
1481}
1482
1483// IOD of SBAS Ephemeris (virtual)
1484////////////////////////////////////////////////////////////////////////////
1485
1486unsigned int t_ephSBAS::IOD() const {
1487 unsigned char buffer[80];
1488 int size = 0;
1489 int numbits = 0;
1490 long long bitbuffer = 0;
1491 unsigned char *startbuffer = buffer;
1492
1493 SBASADDBITSFLOAT(30, this->_x_pos, 0.08)
1494 SBASADDBITSFLOAT(30, this->_y_pos, 0.08)
1495 SBASADDBITSFLOAT(25, this->_z_pos, 0.4)
1496 SBASADDBITSFLOAT(17, this->_x_velocity, 0.000625)
1497 SBASADDBITSFLOAT(17, this->_y_velocity, 0.000625)
1498 SBASADDBITSFLOAT(18, this->_z_velocity, 0.004)
1499 SBASADDBITSFLOAT(10, this->_x_acceleration, 0.0000125)
1500 SBASADDBITSFLOAT(10, this->_y_acceleration, 0.0000125)
1501 SBASADDBITSFLOAT(10, this->_z_acceleration, 0.0000625)
1502 SBASADDBITSFLOAT(12, this->_agf0, 1.0/static_cast<double>(1<<30)/static_cast<double>(1<<1))
1503 SBASADDBITSFLOAT(8, this->_agf1, 1.0/static_cast<double>(1<<30)/static_cast<double>(1<<10))
1504 SBASADDBITS(5,0); // the last byte is filled by 0-bits to obtain a length of an integer multiple of 8
1505
1506 return CRC24(size, startbuffer);
1507}
1508
1509// Compute SBAS Satellite Position (virtual)
1510////////////////////////////////////////////////////////////////////////////
1511t_irc t_ephSBAS::position(int GPSweek, double GPSweeks, double* xc, double* vv) const {
1512
1513 bncTime tt(GPSweek, GPSweeks);
1514 double dt = tt - _TOC;
1515
1516 xc[0] = _x_pos + _x_velocity * dt + _x_acceleration * dt * dt / 2.0;
1517 xc[1] = _y_pos + _y_velocity * dt + _y_acceleration * dt * dt / 2.0;
1518 xc[2] = _z_pos + _z_velocity * dt + _z_acceleration * dt * dt / 2.0;
1519
1520 vv[0] = _x_velocity + _x_acceleration * dt;
1521 vv[1] = _y_velocity + _y_acceleration * dt;
1522 vv[2] = _z_velocity + _z_acceleration * dt;
1523
1524 xc[3] = _agf0 + _agf1 * dt;
1525
1526 xc[4] = _agf1;
1527 xc[5] = 0.0;
1528
1529 return success;
1530}
1531
1532// Health status of SBAS Ephemeris (virtual)
1533////////////////////////////////////////////////////////////////////////////
1534unsigned int t_ephSBAS::isUnhealthy() const {
1535
1536 // Bit 5
1537 bool URAindexIs15 = (int(_health) & (1<<5));
1538 if (URAindexIs15) {
1539 // in this case it is recommended
1540 // to set the bits 0,1,2,3 to 1 (MT17health = 15)
1541 return 1;
1542 }
1543
1544 // Bit 0-3
1545 int MT17health = (int(_health)) & (0x0f);
1546 if (MT17health) {
1547 return 1;
1548 }
1549
1550 // Bit 4
1551 // bool MT17HealthIsUnavailable = (int(_health) & (1<<4));
1552 // is not used because the MT17health bits can be independently set if URA index is 15
1553
1554 return 0;
1555}
1556
1557
1558// RINEX Format String
1559//////////////////////////////////////////////////////////////////////////////
1560QString t_ephSBAS::toString(double version) const {
1561
1562 QString navStr = navTypeString(_navType, _prn, version);
1563 QString rnxStr = navStr + rinexDateStr(_TOC, _prn, version);
1564
1565 QTextStream out(&rnxStr);
1566
1567 out << QString("%1%2%3\n")
1568 .arg(_agf0, 19, 'e', 12)
1569 .arg(_agf1, 19, 'e', 12)
1570 .arg(_TOT, 19, 'e', 12);
1571
1572 QString fmt = version < 3.0 ? " %1%2%3%4\n" : " %1%2%3%4\n";
1573
1574 out << QString(fmt)
1575 .arg(1.e-3*_x_pos, 19, 'e', 12)
1576 .arg(1.e-3*_x_velocity, 19, 'e', 12)
1577 .arg(1.e-3*_x_acceleration, 19, 'e', 12)
1578 .arg(_health, 19, 'e', 12);
1579
1580 out << QString(fmt)
1581 .arg(1.e-3*_y_pos, 19, 'e', 12)
1582 .arg(1.e-3*_y_velocity, 19, 'e', 12)
1583 .arg(1.e-3*_y_acceleration, 19, 'e', 12)
1584 .arg(_ura, 19, 'e', 12);
1585
1586 out << QString(fmt)
1587 .arg(1.e-3*_z_pos, 19, 'e', 12)
1588 .arg(1.e-3*_z_velocity, 19, 'e', 12)
1589 .arg(1.e-3*_z_acceleration, 19, 'e', 12)
1590 .arg(double(_IODN), 19, 'e', 12);
1591
1592 return rnxStr;
1593}
1594
1595// Constructor
1596//////////////////////////////////////////////////////////////////////////////
1597t_ephBDS::t_ephBDS(double rnxVersion, const QStringList& lines) {
1598
1599 const int nLines = 8;
1600
1601 if (lines.size() != nLines) {
1602 _checkState = bad;
1603 return;
1604 }
1605
1606 // RINEX Format
1607 // ------------
1608 int fieldLen = 19;
1609
1610 int pos[4];
1611 pos[0] = (rnxVersion <= 2.12) ? 3 : 4;
1612 pos[1] = pos[0] + fieldLen;
1613 pos[2] = pos[1] + fieldLen;
1614 pos[3] = pos[2] + fieldLen;
1615
1616 // Read eight lines
1617 // ----------------
1618 for (int iLine = 0; iLine < nLines; iLine++) {
1619 QString line = lines[iLine];
1620
1621 if ( iLine == 0 ) {
1622 QTextStream in(line.left(pos[1]).toLatin1());
1623
1624 int year, month, day, hour, min;
1625 double sec;
1626
1627 QString prnStr, n;
1628 in >> prnStr;
1629 if (prnStr.size() == 1 && prnStr[0] == 'C') {
1630 in >> n;
1631 prnStr.append(n);
1632 }
1633 in >> year >> month >> day >> hour >> min >> sec;
1634 if (prnStr.at(0) == 'C') {
1635 _prn.set('C', prnStr.mid(1).toInt());
1636 }
1637 else {
1638 _prn.set('C', prnStr.toInt());
1639 }
1640
1641 if (year < 80) {
1642 year += 2000;
1643 }
1644 else if (year < 100) {
1645 year += 1900;
1646 }
1647
1648 _TOC.setBDS(year, month, day, hour, min, sec);
1649
1650 if ( readDbl(line, pos[1], fieldLen, _clock_bias ) ||
1651 readDbl(line, pos[2], fieldLen, _clock_drift ) ||
1652 readDbl(line, pos[3], fieldLen, _clock_driftrate) ) {
1653 _checkState = bad;
1654 return;
1655 }
1656 }
1657
1658 else if ( iLine == 1 ) {
1659 double aode;
1660 if ( readDbl(line, pos[0], fieldLen, aode ) ||
1661 readDbl(line, pos[1], fieldLen, _Crs ) ||
1662 readDbl(line, pos[2], fieldLen, _Delta_n) ||
1663 readDbl(line, pos[3], fieldLen, _M0 ) ) {
1664 _checkState = bad;
1665 return;
1666 }
1667 _AODE = int(aode);
1668 }
1669
1670 else if ( iLine == 2 ) {
1671 if ( readDbl(line, pos[0], fieldLen, _Cuc ) ||
1672 readDbl(line, pos[1], fieldLen, _e ) ||
1673 readDbl(line, pos[2], fieldLen, _Cus ) ||
1674 readDbl(line, pos[3], fieldLen, _sqrt_A) ) {
1675 _checkState = bad;
1676 return;
1677 }
1678 }
1679
1680 else if ( iLine == 3 ) {
1681 if ( readDbl(line, pos[0], fieldLen, _TOEsec ) ||
1682 readDbl(line, pos[1], fieldLen, _Cic ) ||
1683 readDbl(line, pos[2], fieldLen, _OMEGA0) ||
1684 readDbl(line, pos[3], fieldLen, _Cis ) ) {
1685 _checkState = bad;
1686 return;
1687 }
1688 }
1689
1690 else if ( iLine == 4 ) {
1691 if ( readDbl(line, pos[0], fieldLen, _i0 ) ||
1692 readDbl(line, pos[1], fieldLen, _Crc ) ||
1693 readDbl(line, pos[2], fieldLen, _omega ) ||
1694 readDbl(line, pos[3], fieldLen, _OMEGADOT) ) {
1695 _checkState = bad;
1696 return;
1697 }
1698 }
1699
1700 else if ( iLine == 5 ) {
1701 if ( readDbl(line, pos[0], fieldLen, _IDOT ) ||
1702 readDbl(line, pos[2], fieldLen, _TOEweek)) {
1703 _checkState = bad;
1704 return;
1705 }
1706 }
1707
1708 else if ( iLine == 6 ) {
1709 double SatH1;
1710 if ( readDbl(line, pos[0], fieldLen, _URA ) ||
1711 readDbl(line, pos[1], fieldLen, SatH1) ||
1712 readDbl(line, pos[2], fieldLen, _TGD1) ||
1713 readDbl(line, pos[3], fieldLen, _TGD2) ) {
1714 _checkState = bad;
1715 return;
1716 }
1717 _SatH1 = int(SatH1);
1718 }
1719
1720 else if ( iLine == 7 ) {
1721 double aodc;
1722 if ( readDbl(line, pos[0], fieldLen, _TOT) ||
1723 readDbl(line, pos[1], fieldLen, aodc) ) {
1724 _checkState = bad;
1725 return;
1726 }
1727 if (_TOT == 0.9999e9) { // 0.9999e9 means not known (RINEX standard)
1728 _TOT = _TOEsec;
1729 }
1730 _AODC = int(aodc);
1731 }
1732 }
1733
1734 _TOE.setBDS(int(_TOEweek), _TOEsec);
1735
1736 // remark: actually should be computed from second_tot
1737 // but it seems to be unreliable in RINEX files
1738 //_TOT = _TOC.bdssec();
1739}
1740
1741// IOD of BDS Ephemeris (virtual)
1742////////////////////////////////////////////////////////////////////////////
1743unsigned int t_ephBDS::IOD() const {
1744 return (int(_TOEsec)/720) % 240;
1745}
1746
1747// Compute BDS Satellite Position (virtual)
1748//////////////////////////////////////////////////////////////////////////////
1749t_irc t_ephBDS::position(int GPSweek, double GPSweeks, double* xc, double* vv) const {
1750
1751 static const double gmBDS = 398.6004418e12;
1752 static const double omegaBDS = 7292115.0000e-11;
1753
1754 xc[0] = xc[1] = xc[2] = xc[3] = 0.0;
1755 vv[0] = vv[1] = vv[2] = 0.0;
1756
1757 bncTime tt(GPSweek, GPSweeks);
1758
1759 if (_sqrt_A == 0) {
1760 return failure;
1761 }
1762 double a0 = _sqrt_A * _sqrt_A;
1763
1764 double n0 = sqrt(gmBDS/(a0*a0*a0));
1765 double tk = tt - _TOE;
1766 double n = n0 + _Delta_n;
1767 double M = _M0 + n*tk;
1768 double E = M;
1769 double E_last;
1770 int nLoop = 0;
1771 do {
1772 E_last = E;
1773 E = M + _e*sin(E);
1774
1775 if (++nLoop == 100) {
1776 return failure;
1777 }
1778 } while ( fabs(E-E_last)*a0 > 0.001 );
1779
1780 double v = atan2(sqrt(1-_e*_e) * sin(E), cos(E) - _e);
1781 double u0 = v + _omega;
1782 double sin2u0 = sin(2*u0);
1783 double cos2u0 = cos(2*u0);
1784 double r = a0*(1 - _e*cos(E)) + _Crc*cos2u0 + _Crs*sin2u0;
1785 double i = _i0 + _IDOT*tk + _Cic*cos2u0 + _Cis*sin2u0;
1786 double u = u0 + _Cuc*cos2u0 + _Cus*sin2u0;
1787 double xp = r*cos(u);
1788 double yp = r*sin(u);
1789 double toesec = (_TOE.gpssec() - 14.0);
1790 double sinom = 0;
1791 double cosom = 0;
1792 double sini = 0;
1793 double cosi = 0;
1794
1795 // Velocity
1796 // --------
1797 double tanv2 = tan(v/2);
1798 double dEdM = 1 / (1 - _e*cos(E));
1799 double dotv = sqrt((1.0 + _e)/(1.0 - _e)) / cos(E/2)/cos(E/2)
1800 / (1 + tanv2*tanv2) * dEdM * n;
1801 double dotu = dotv + (-_Cuc*sin2u0 + _Cus*cos2u0)*2*dotv;
1802 double doti = _IDOT + (-_Cic*sin2u0 + _Cis*cos2u0)*2*dotv;
1803 double dotr = a0 * _e*sin(E) * dEdM * n
1804 + (-_Crc*sin2u0 + _Crs*cos2u0)*2*dotv;
1805
1806 double dotx = dotr*cos(u) - r*sin(u)*dotu;
1807 double doty = dotr*sin(u) + r*cos(u)*dotu;
1808
1809 const double iMaxGEO = 10.0 / 180.0 * M_PI;
1810
1811 // MEO/IGSO satellite
1812 // ------------------
1813 if (_i0 > iMaxGEO) {
1814 double OM = _OMEGA0 + (_OMEGADOT - omegaBDS)*tk - omegaBDS*toesec;
1815
1816 sinom = sin(OM);
1817 cosom = cos(OM);
1818 sini = sin(i);
1819 cosi = cos(i);
1820
1821 xc[0] = xp*cosom - yp*cosi*sinom;
1822 xc[1] = xp*sinom + yp*cosi*cosom;
1823 xc[2] = yp*sini;
1824
1825 // Velocity
1826 // --------
1827
1828 double dotom = _OMEGADOT - t_CST::omega;
1829
1830 vv[0] = cosom *dotx - cosi*sinom *doty // dX / dr
1831 - xp*sinom*dotom - yp*cosi*cosom*dotom // dX / dOMEGA
1832 + yp*sini*sinom*doti; // dX / di
1833
1834 vv[1] = sinom *dotx + cosi*cosom *doty
1835 + xp*cosom*dotom - yp*cosi*sinom*dotom
1836 - yp*sini*cosom*doti;
1837
1838 vv[2] = sini *doty + yp*cosi *doti;
1839
1840 }
1841
1842 // GEO satellite
1843 // -------------
1844 else {
1845 double OM = _OMEGA0 + _OMEGADOT*tk - omegaBDS*toesec;
1846 double ll = omegaBDS*tk;
1847
1848 sinom = sin(OM);
1849 cosom = cos(OM);
1850 sini = sin(i);
1851 cosi = cos(i);
1852
1853 double xx = xp*cosom - yp*cosi*sinom;
1854 double yy = xp*sinom + yp*cosi*cosom;
1855 double zz = yp*sini;
1856
1857 Matrix RX = BNC_PPP::t_astro::rotX(-5.0 / 180.0 * M_PI);
1858 Matrix RZ = BNC_PPP::t_astro::rotZ(ll);
1859
1860 ColumnVector X1(3); X1 << xx << yy << zz;
1861 ColumnVector X2 = RZ*RX*X1;
1862
1863 xc[0] = X2(1);
1864 xc[1] = X2(2);
1865 xc[2] = X2(3);
1866
1867 double dotom = _OMEGADOT;
1868
1869 double vx = cosom *dotx - cosi*sinom *doty
1870 - xp*sinom*dotom - yp*cosi*cosom*dotom
1871 + yp*sini*sinom*doti;
1872
1873 double vy = sinom *dotx + cosi*cosom *doty
1874 + xp*cosom*dotom - yp*cosi*sinom*dotom
1875 - yp*sini*cosom*doti;
1876
1877 double vz = sini *doty + yp*cosi *doti;
1878
1879 ColumnVector V(3); V << vx << vy << vz;
1880
1881 Matrix RdotZ(3,3);
1882 double C = cos(ll);
1883 double S = sin(ll);
1884 Matrix UU(3,3);
1885 UU[0][0] = -S; UU[0][1] = +C; UU[0][2] = 0.0;
1886 UU[1][0] = -C; UU[1][1] = -S; UU[1][2] = 0.0;
1887 UU[2][0] = 0.0; UU[2][1] = 0.0; UU[2][2] = 0.0;
1888 RdotZ = omegaBDS * UU;
1889
1890 ColumnVector VV(3);
1891 VV = RZ*RX*V + RdotZ*RX*X1;
1892
1893 vv[0] = VV(1);
1894 vv[1] = VV(2);
1895 vv[2] = VV(3);
1896 }
1897
1898 double tc = tt - _TOC;
1899 xc[3] = _clock_bias + _clock_drift*tc + _clock_driftrate*tc*tc;
1900
1901// dotC = _clock_drift + _clock_driftrate*tc
1902// - 4.442807309e-10*_e * sqrt(a0) * cos(E) * dEdM * n;
1903
1904 // Relativistic Correction
1905 // -----------------------
1906 xc[3] -= 4.442807309e-10 * _e * sqrt(a0) *sin(E);
1907
1908 xc[4] = _clock_drift + _clock_driftrate*tc;
1909 xc[5] = _clock_driftrate;
1910
1911 return success;
1912}
1913
1914// RINEX Format String
1915//////////////////////////////////////////////////////////////////////////////
1916QString t_ephBDS::toString(double version) const {
1917
1918 QString navStr = navTypeString(_navType, _prn, version);
1919 QString rnxStr = navStr + rinexDateStr(_TOC-14.0, _prn, version);
1920
1921 QTextStream out(&rnxStr);
1922
1923 out << QString("%1%2%3\n")
1924 .arg(_clock_bias, 19, 'e', 12)
1925 .arg(_clock_drift, 19, 'e', 12)
1926 .arg(_clock_driftrate, 19, 'e', 12);
1927
1928 QString fmt = version < 3.0 ? " %1%2%3%4\n" : " %1%2%3%4\n";
1929
1930 out << QString(fmt)
1931 .arg(double(_AODE), 19, 'e', 12)
1932 .arg(_Crs, 19, 'e', 12)
1933 .arg(_Delta_n, 19, 'e', 12)
1934 .arg(_M0, 19, 'e', 12);
1935
1936 out << QString(fmt)
1937 .arg(_Cuc, 19, 'e', 12)
1938 .arg(_e, 19, 'e', 12)
1939 .arg(_Cus, 19, 'e', 12)
1940 .arg(_sqrt_A, 19, 'e', 12);
1941
1942 double toes = 0.0;
1943 if (_TOEweek > -1.0) {// RINEX input
1944 toes = _TOEsec;
1945 }
1946 else {// RTCM stream input
1947 toes = _TOE.bdssec();
1948 }
1949 out << QString(fmt)
1950 .arg(toes, 19, 'e', 12)
1951 .arg(_Cic, 19, 'e', 12)
1952 .arg(_OMEGA0, 19, 'e', 12)
1953 .arg(_Cis, 19, 'e', 12);
1954
1955 out << QString(fmt)
1956 .arg(_i0, 19, 'e', 12)
1957 .arg(_Crc, 19, 'e', 12)
1958 .arg(_omega, 19, 'e', 12)
1959 .arg(_OMEGADOT, 19, 'e', 12);
1960
1961 double toew = 0.0;
1962 if (_TOEweek > -1.0) {// RINEX input
1963 toew = _TOEweek;
1964 }
1965 else {// RTCM stream input
1966 toew = double(_TOE.bdsw());
1967 }
1968 out << QString(fmt)
1969 .arg(_IDOT, 19, 'e', 12)
1970 .arg(0.0, 19, 'e', 12)
1971 .arg(toew, 19, 'e', 12)
1972 .arg(0.0, 19, 'e', 12);
1973
1974 out << QString(fmt)
1975 .arg(_URA, 19, 'e', 12)
1976 .arg(double(_SatH1), 19, 'e', 12)
1977 .arg(_TGD1, 19, 'e', 12)
1978 .arg(_TGD2, 19, 'e', 12);
1979
1980 double tots = 0.0;
1981 if (_TOEweek > -1.0) {// RINEX input
1982 tots = _TOT;
1983 }
1984 else {// RTCM stream input
1985 tots = _TOE.bdssec();
1986 }
1987 out << QString(fmt)
1988 .arg(tots, 19, 'e', 12)
1989 .arg(double(_AODC), 19, 'e', 12)
1990 .arg("", 19, QChar(' '))
1991 .arg("", 19, QChar(' '));
1992 return rnxStr;
1993}
Note: See TracBrowser for help on using the repository browser.