[758] | 1 | /* -------------------------------------------------------------------------
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| 2 | * BKG NTRIP Server
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| 3 | * -------------------------------------------------------------------------
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| 4 | *
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| 5 | * Class: bnseph
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| 6 | *
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| 7 | * Purpose: Retrieve broadcast ephemeris from BNC
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| 8 | *
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| 9 | * Author: L. Mervart
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| 10 | *
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| 11 | * Created: 29-Mar-2008
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| 12 | *
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| 13 | * Changes:
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| 14 | *
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| 15 | * -----------------------------------------------------------------------*/
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| 16 |
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[761] | 17 | #include <iostream>
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[776] | 18 | #include <math.h>
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[761] | 19 |
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[758] | 20 | #include "bnseph.h"
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[776] | 21 | #include "bnsutils.h"
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[758] | 22 |
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| 23 | using namespace std;
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| 24 |
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| 25 | // Constructor
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| 26 | ////////////////////////////////////////////////////////////////////////////
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| 27 | t_bnseph::t_bnseph(QObject* parent) : QThread(parent) {
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[839] | 28 |
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| 29 | this->setTerminationEnabled(true);
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| 30 |
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[830] | 31 | _socket = 0;
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[758] | 32 | }
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| 33 |
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| 34 | // Destructor
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| 35 | ////////////////////////////////////////////////////////////////////////////
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| 36 | t_bnseph::~t_bnseph() {
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[759] | 37 | delete _socket;
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[758] | 38 | }
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| 39 |
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[838] | 40 | // Connect the Socket
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[758] | 41 | ////////////////////////////////////////////////////////////////////////////
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[838] | 42 | void t_bnseph::reconnect() {
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[759] | 43 |
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[838] | 44 | delete _socket;
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[759] | 45 |
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[830] | 46 | QSettings settings;
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| 47 | QString host = "localhost";
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| 48 | int port = settings.value("ephPort").toInt();
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| 49 |
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| 50 | _socket = new QTcpSocket();
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| 51 | _socket->connectToHost(host, port);
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| 52 |
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[838] | 53 | const int timeOut = 10*1000; // 10 seconds
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[830] | 54 | if (!_socket->waitForConnected(timeOut)) {
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[838] | 55 | emit(newMessage("bnseph::run Connect Timeout"));
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[830] | 56 | }
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[838] | 57 | }
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| 58 |
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| 59 | // Start
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| 60 | ////////////////////////////////////////////////////////////////////////////
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| 61 | void t_bnseph::run() {
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| 62 |
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| 63 | emit(newMessage("bnseph::run Start"));
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| 64 |
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| 65 | while (true) {
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| 66 | if (_socket == 0 || _socket->state() != QAbstractSocket::ConnectedState) {
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| 67 | reconnect();
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| 68 | }
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| 69 | if (_socket && _socket->state() == QAbstractSocket::ConnectedState) {
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[830] | 70 | if (_socket->canReadLine()) {
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| 71 | readEph();
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| 72 | }
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| 73 | else {
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| 74 | _socket->waitForReadyRead(10);
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| 75 | }
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[759] | 76 | }
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[838] | 77 | else {
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| 78 | msleep(10);
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| 79 | }
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[759] | 80 | }
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[758] | 81 | }
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| 82 |
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[771] | 83 | // Read One Ephemeris
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| 84 | ////////////////////////////////////////////////////////////////////////////
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| 85 | void t_bnseph::readEph() {
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| 86 |
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| 87 |
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[884] | 88 | t_eph* eph = 0;
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[782] | 89 |
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[884] | 90 | QByteArray line = _socket->readLine();
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| 91 | QTextStream in(line);
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| 92 | QString prn;
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| 93 |
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| 94 | in >> prn;
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[771] | 95 |
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[884] | 96 | int numlines = 0;
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| 97 | if (prn.indexOf('R') != -1) {
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| 98 | eph = new t_ephGlo();
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| 99 | numlines = 4;
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| 100 | }
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| 101 | else {
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| 102 | eph = new t_ephGPS();
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| 103 | numlines = 8;
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| 104 | }
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[771] | 105 |
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[884] | 106 | QStringList lines;
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| 107 | lines << line;
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| 108 |
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| 109 | for (int ii = 2; ii <= numlines; ii++) {
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[781] | 110 | QByteArray line = _socket->readLine();
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[884] | 111 | lines << line;
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| 112 | }
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[782] | 113 |
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[884] | 114 | eph->read(lines);
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[782] | 115 |
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[884] | 116 | emit(newEph(eph));
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| 117 | }
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[778] | 118 |
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[886] | 119 | // Compare Time
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| 120 | ////////////////////////////////////////////////////////////////////////////
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| 121 | bool t_eph::isNewerThan(const t_eph* eph) const {
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| 122 | if (_GPSweek > eph->_GPSweek ||
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| 123 | (_GPSweek == eph->_GPSweek && _GPSweeks > eph->_GPSweeks)) {
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| 124 | return true;
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| 125 | }
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| 126 | else {
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| 127 | return false;
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| 128 | }
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| 129 | }
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| 130 |
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[884] | 131 | // Read GPS Ephemeris
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| 132 | ////////////////////////////////////////////////////////////////////////////
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| 133 | void t_ephGPS::read(const QStringList& lines) {
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[782] | 134 |
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[884] | 135 | for (int ii = 1; ii <= lines.size(); ii++) {
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| 136 | QTextStream in(lines.at(ii-1).toAscii());
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[782] | 137 |
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[884] | 138 | if (ii == 1) {
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[800] | 139 | double year, month, day, hour, minute, second;
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[884] | 140 | in >> _prn >> year >> month >> day >> hour >> minute >> second
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| 141 | >> _clock_bias >> _clock_drift >> _clock_driftrate;
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[781] | 142 |
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| 143 | if (year < 100) year += 2000;
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| 144 |
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[805] | 145 | QDateTime dateTime(QDate(int(year), int(month), int(day)),
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| 146 | QTime(int(hour), int(minute), int(second)), Qt::UTC);
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[886] | 147 |
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| 148 | GPSweekFromDateAndTime(dateTime, _GPSweek, _GPSweeks);
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| 149 | _TOC = _GPSweeks;
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[781] | 150 | }
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| 151 | else if (ii == 2) {
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[884] | 152 | in >> _IODE >> _Crs >> _Delta_n >> _M0;
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[781] | 153 | }
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| 154 | else if (ii == 3) {
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[884] | 155 | in >> _Cuc >> _e >> _Cus >> _sqrt_A;
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[781] | 156 | }
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| 157 | else if (ii == 4) {
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[884] | 158 | in >> _TOE >> _Cic >> _OMEGA0 >> _Cis;
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[781] | 159 | }
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| 160 | else if (ii == 5) {
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[884] | 161 | in >> _i0 >> _Crc >> _omega >> _OMEGADOT;
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[781] | 162 | }
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| 163 | else if (ii == 6) {
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[884] | 164 | in >> _IDOT;
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[781] | 165 | }
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| 166 | else if (ii == 7) {
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[800] | 167 | double hlp, health;
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[884] | 168 | in >> hlp >> health >> _TGD >> _IODC;
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[781] | 169 | }
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| 170 | else if (ii == 8) {
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[884] | 171 | in >> _TOW;
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[781] | 172 | }
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| 173 | }
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[884] | 174 | }
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[773] | 175 |
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[884] | 176 | // Compute GPS Satellite Position
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| 177 | ////////////////////////////////////////////////////////////////////////////
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| 178 | void t_ephGPS::position(int GPSweek, double GPSweeks, ColumnVector& xc,
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| 179 | ColumnVector& vv) const {
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| 180 |
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| 181 | const static double secPerWeek = 7 * 86400.0;
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| 182 | const static double omegaEarth = 7292115.1467e-11;
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| 183 | const static double gmWGS = 398.6005e12;
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| 184 |
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| 185 | if (xc.Nrows() < 4) {
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| 186 | xc.ReSize(4);
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| 187 | }
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| 188 | xc = 0.0;
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| 189 |
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| 190 | if (vv.Nrows() < 3) {
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| 191 | vv.ReSize(3);
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| 192 | }
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| 193 | vv = 0.0;
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| 194 |
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| 195 | double a0 = _sqrt_A * _sqrt_A;
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| 196 | if (a0 == 0) {
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| 197 | return;
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| 198 | }
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| 199 |
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| 200 | double n0 = sqrt(gmWGS/(a0*a0*a0));
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| 201 | double tk = GPSweeks - _TOE;
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| 202 | if (GPSweek != _GPSweek) {
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| 203 | tk += (GPSweek - _GPSweek) * secPerWeek;
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| 204 | }
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| 205 | double n = n0 + _Delta_n;
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| 206 | double M = _M0 + n*tk;
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| 207 | double E = M;
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| 208 | double E_last;
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| 209 | do {
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| 210 | E_last = E;
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| 211 | E = M + _e*sin(E);
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| 212 | } while ( fabs(E-E_last)*a0 > 0.001 );
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| 213 | double v = 2.0*atan( sqrt( (1.0 + _e)/(1.0 - _e) )*tan( E/2 ) );
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| 214 | double u0 = v + _omega;
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| 215 | double sin2u0 = sin(2*u0);
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| 216 | double cos2u0 = cos(2*u0);
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| 217 | double r = a0*(1 - _e*cos(E)) + _Crc*cos2u0 + _Crs*sin2u0;
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| 218 | double i = _i0 + _IDOT*tk + _Cic*cos2u0 + _Cis*sin2u0;
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| 219 | double u = u0 + _Cuc*cos2u0 + _Cus*sin2u0;
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| 220 | double xp = r*cos(u);
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| 221 | double yp = r*sin(u);
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| 222 | double OM = _OMEGA0 + (_OMEGADOT - omegaEarth)*tk -
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| 223 | omegaEarth*_TOE;
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| 224 |
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| 225 | double sinom = sin(OM);
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| 226 | double cosom = cos(OM);
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| 227 | double sini = sin(i);
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| 228 | double cosi = cos(i);
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| 229 | xc(1) = xp*cosom - yp*cosi*sinom;
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| 230 | xc(2) = xp*sinom + yp*cosi*cosom;
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| 231 | xc(3) = yp*sini;
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| 232 |
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| 233 | double tc = GPSweeks - _TOC;
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| 234 | if (GPSweek != _GPSweek) {
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| 235 | tc += (GPSweek - _GPSweek) * secPerWeek;
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| 236 | }
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| 237 | xc(4) = _clock_bias + _clock_drift*tc + _clock_driftrate*tc*tc
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| 238 | - 4.442807633e-10 * _e * sqrt(a0) *sin(E);
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| 239 |
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| 240 | // Velocity
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| 241 | // --------
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| 242 | double tanv2 = tan(v/2);
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| 243 | double dEdM = 1 / (1 - _e*cos(E));
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| 244 | double dotv = sqrt((1.0 + _e)/(1.0 - _e)) / cos(E/2)/cos(E/2) / (1 + tanv2*tanv2)
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| 245 | * dEdM * n;
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| 246 | double dotu = dotv + (-_Cuc*sin2u0 + _Cus*cos2u0)*2*dotv;
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| 247 | double dotom = _OMEGADOT - omegaEarth;
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| 248 | double doti = _IDOT + (-_Cic*sin2u0 + _Cis*cos2u0)*2*dotv;
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| 249 | double dotr = a0 * _e*sin(E) * dEdM * n
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| 250 | + (-_Crc*sin2u0 + _Crs*cos2u0)*2*dotv;
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| 251 | double dotx = dotr*cos(u) - r*sin(u)*dotu;
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| 252 | double doty = dotr*sin(u) + r*cos(u)*dotu;
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| 253 |
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| 254 | vv(1) = cosom *dotx - cosi*sinom *doty // dX / dr
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| 255 | - xp*sinom*dotom - yp*cosi*cosom*dotom // dX / dOMEGA
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| 256 | + yp*sini*sinom*doti; // dX / di
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| 257 |
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| 258 | vv(2) = sinom *dotx + cosi*cosom *doty
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| 259 | + xp*cosom*dotom - yp*cosi*sinom*dotom
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| 260 | - yp*sini*cosom*doti;
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| 261 |
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| 262 | vv(3) = sini *doty + yp*cosi *doti;
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[771] | 263 | }
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[884] | 264 |
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[889] | 265 | // Read Glonass Ephemeris
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[884] | 266 | ////////////////////////////////////////////////////////////////////////////
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| 267 | void t_ephGlo::read(const QStringList& lines) {
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| 268 |
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| 269 | for (int ii = 1; ii <= lines.size(); ii++) {
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| 270 | QTextStream in(lines.at(ii-1).toAscii());
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| 271 |
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| 272 | if (ii == 1) {
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| 273 | double year, month, day, hour, minute, second;
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| 274 | in >> _prn >> year >> month >> day >> hour >> minute >> second
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| 275 | >> _tau >> _gamma;
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[886] | 276 |
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| 277 | _tau = -_tau;
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[884] | 278 |
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| 279 | if (year < 100) year += 2000;
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| 280 |
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| 281 | QDateTime dateTime(QDate(int(year), int(month), int(day)),
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| 282 | QTime(int(hour), int(minute), int(second)), Qt::UTC);
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[886] | 283 |
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| 284 | GPSweekFromDateAndTime(dateTime, _GPSweek, _GPSweeks);
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[910] | 285 |
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[911] | 286 | //// beg test
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| 287 | _gps_utc = 14.0;
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| 288 | //// end test
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| 289 |
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[910] | 290 | _GPSweeks += _gps_utc;
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[884] | 291 | }
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| 292 | else if (ii == 2) {
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[886] | 293 | in >>_x_pos >> _x_velocity >> _x_acceleration >> _health;
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[884] | 294 | }
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| 295 | else if (ii == 3) {
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| 296 | in >>_y_pos >> _y_velocity >> _y_acceleration >> _frequency_number;
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| 297 | }
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| 298 | else if (ii == 4) {
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| 299 | in >>_z_pos >> _z_velocity >> _z_acceleration >> _E;
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| 300 | }
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| 301 | }
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| 302 |
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[888] | 303 | // Initialize status vector
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| 304 | // ------------------------
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[901] | 305 | _tt = _GPSweeks;
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[888] | 306 |
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[893] | 307 | _xv(1) = _x_pos * 1.e3;
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| 308 | _xv(2) = _y_pos * 1.e3;
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| 309 | _xv(3) = _z_pos * 1.e3;
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| 310 | _xv(4) = _x_velocity * 1.e3;
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| 311 | _xv(5) = _y_velocity * 1.e3;
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| 312 | _xv(6) = _z_velocity * 1.e3;
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[884] | 313 | }
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| 314 |
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| 315 | // Derivative of the state vector using a simple force model (static)
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| 316 | ////////////////////////////////////////////////////////////////////////////
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| 317 | ColumnVector t_ephGlo::glo_deriv(double /* tt */, const ColumnVector& xv) {
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| 318 |
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| 319 | // State vector components
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| 320 | // -----------------------
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| 321 | ColumnVector rr = xv.rows(1,3);
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| 322 | ColumnVector vv = xv.rows(4,6);
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| 323 |
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| 324 | // Acceleration
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| 325 | // ------------
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| 326 | const static double GM = 398.60044e12;
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| 327 | const static double AE = 6378136.0;
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| 328 | const static double OMEGA = 7292115.e-11;
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| 329 | const static double C20 = -1082.63e-6;
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| 330 |
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| 331 | double rho = rr.norm_Frobenius();
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| 332 | double t1 = -GM/(rho*rho*rho);
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| 333 | double t2 = 3.0/2.0 * C20 * (GM*AE*AE) / (rho*rho*rho*rho*rho);
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| 334 | double t3 = OMEGA * OMEGA;
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| 335 | double t4 = 2.0 * OMEGA;
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| 336 | double z2 = rr(3) * rr(3);
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| 337 |
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| 338 | // Vector of derivatives
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| 339 | // ---------------------
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| 340 | ColumnVector va(6);
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| 341 | va(1) = vv(1);
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| 342 | va(2) = vv(2);
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| 343 | va(3) = vv(3);
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| 344 | va(4) = (t1 + t2*(1.0-5.0*z2/(rho*rho)) + t3) * rr(1) + t4*vv(2);
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| 345 | va(5) = (t1 + t2*(1.0-5.0*z2/(rho*rho)) + t3) * rr(2) - t4*vv(1);
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| 346 | va(6) = (t1 + t2*(3.0-5.0*z2/(rho*rho)) ) * rr(3);
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| 347 |
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| 348 | return va;
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| 349 | }
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| 350 |
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[889] | 351 | // Compute Glonass Satellite Position
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[884] | 352 | ////////////////////////////////////////////////////////////////////////////
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| 353 | void t_ephGlo::position(int GPSweek, double GPSweeks, ColumnVector& xc,
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| 354 | ColumnVector& vv) const {
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| 355 |
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[899] | 356 | const static double secPerWeek = 7 * 86400.0;
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| 357 | const static double nominalStep = 10.0;
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[891] | 358 |
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[898] | 359 | double dtPos = GPSweeks - _tt;
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[891] | 360 | if (GPSweek != _GPSweek) {
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[898] | 361 | dtPos += (GPSweek - _GPSweek) * secPerWeek;
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[891] | 362 | }
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| 363 |
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[899] | 364 | int nSteps = int(fabs(dtPos) / nominalStep) + 1;
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| 365 | double step = dtPos / nSteps;
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| 366 |
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| 367 | for (int ii = 1; ii <= nSteps; ii++) {
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[900] | 368 | _xv = rungeKutta4(_tt, _xv, step, glo_deriv);
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[899] | 369 | _tt += step;
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[891] | 370 | }
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| 371 |
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[892] | 372 | // Position and Velocity
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| 373 | // ---------------------
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[891] | 374 | xc(1) = _xv(1);
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| 375 | xc(2) = _xv(2);
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| 376 | xc(3) = _xv(3);
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| 377 |
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| 378 | vv(1) = _xv(4);
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| 379 | vv(2) = _xv(5);
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| 380 | vv(3) = _xv(6);
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[892] | 381 |
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| 382 | // Clock Correction
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| 383 | // ----------------
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| 384 | double dtClk = GPSweeks - _GPSweeks;
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| 385 | if (GPSweek != _GPSweek) {
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| 386 | dtClk += (GPSweek - _GPSweek) * secPerWeek;
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| 387 | }
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[910] | 388 | xc(4) = -_tau + _gamma * dtClk;
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[911] | 389 |
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| 390 | cout << _tau << " " << _gamma << " " << dtClk << " " << xc(4) << endl;
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[884] | 391 | }
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| 392 |
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