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https://github.com/gnss-sdr/gnss-sdr
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Remove duplicated code
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@ -338,7 +338,7 @@ bool hybrid_ls_pvt::get_PVT(std::map<int, Gnss_Synchro> gnss_observables_map, do
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boost::posix_time::ptime p_time(boost::gregorian::date(1999, 8, 22), t);
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this->set_position_UTC_time(p_time);
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cart2geo(static_cast<double>(rx_position_and_time(0)), static_cast<double>(rx_position_and_time(1)), static_cast<double>(rx_position_and_time(2)), 4);
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cart_to_geo(static_cast<double>(rx_position_and_time(0)), static_cast<double>(rx_position_and_time(1)), static_cast<double>(rx_position_and_time(2)), 4);
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DLOG(INFO) << "Hybrid Position at " << boost::posix_time::to_simple_string(p_time)
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<< " is Lat = " << this->get_latitude() << " [deg], Long = " << this->get_longitude()
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@ -87,49 +87,13 @@ arma::vec Pvt_Solution::rotateSatellite(double const traveltime, const arma::vec
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}
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int Pvt_Solution::cart2geo(double X, double Y, double Z, int elipsoid_selection)
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int Pvt_Solution::cart_to_geo(double X, double Y, double Z, int elipsoid_selection)
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{
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/* Conversion of Cartesian coordinates (X,Y,Z) to geographical
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coordinates (latitude, longitude, h) on a selected reference ellipsoid.
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Choices of Reference Ellipsoid for Geographical Coordinates
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0. International Ellipsoid 1924
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1. International Ellipsoid 1967
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2. World Geodetic System 1972
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3. Geodetic Reference System 1980
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4. World Geodetic System 1984
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*/
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const double a[5] = {6378388.0, 6378160.0, 6378135.0, 6378137.0, 6378137.0};
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const double f[5] = {1.0 / 297.0, 1.0 / 298.247, 1.0 / 298.26, 1.0 / 298.257222101, 1.0 / 298.257223563};
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double lambda = atan2(Y, X);
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double ex2 = (2.0 - f[elipsoid_selection]) * f[elipsoid_selection] / ((1.0 - f[elipsoid_selection]) * (1.0 - f[elipsoid_selection]));
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double c = a[elipsoid_selection] * sqrt(1.0 + ex2);
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double phi = atan(Z / ((sqrt(X * X + Y * Y) * (1.0 - (2.0 - f[elipsoid_selection])) * f[elipsoid_selection])));
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double h = 0.1;
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double oldh = 0.0;
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double N;
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int iterations = 0;
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do
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{
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oldh = h;
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N = c / sqrt(1 + ex2 * (cos(phi) * cos(phi)));
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phi = atan(Z / ((sqrt(X * X + Y * Y) * (1.0 - (2.0 - f[elipsoid_selection]) * f[elipsoid_selection] * N / (N + h)))));
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h = sqrt(X * X + Y * Y) / cos(phi) - N;
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iterations = iterations + 1;
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if (iterations > 100)
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{
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DLOG(WARNING) << "Failed to approximate h with desired precision. h-oldh= " << h - oldh;
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break;
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}
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}
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while (std::abs(h - oldh) > 1.0e-12);
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d_latitude_d = phi * 180.0 / GPS_PI;
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d_longitude_d = lambda * 180.0 / GPS_PI;
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d_height_m = h;
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//todo: refactor this class. Mix of duplicated functions, use either RTKLIB geodetic functions or geofunctions.h
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arma::vec XYZ = {X, Y, Z};
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arma::vec LLH = cart2geo(XYZ, elipsoid_selection);
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d_latitude_d = LLH(0) * 180.0 / GPS_PI;
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d_longitude_d = LLH(1) * 180.0 / GPS_PI;
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d_height_m = LLH(2);
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return 0;
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}
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@ -127,7 +127,7 @@ public:
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* 4 - World Geodetic System 1984.
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*
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*/
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int cart2geo(double X, double Y, double Z, int elipsoid_selection);
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int cart_to_geo(double X, double Y, double Z, int elipsoid_selection);
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/*!
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* \brief Tropospheric correction
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@ -99,6 +99,7 @@ rtklib_solver::rtklib_solver(int nchannels, std::string dump_filename, bool flag
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}
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}
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bool rtklib_solver::save_matfile()
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{
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// READ DUMP FILE
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@ -395,6 +396,7 @@ bool rtklib_solver::save_matfile()
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return true;
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}
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rtklib_solver::~rtklib_solver()
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{
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if (d_dump_file.is_open() == true)
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@ -868,7 +870,7 @@ bool rtklib_solver::get_PVT(const std::map<int, Gnss_Synchro> &gnss_observables_
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p_time = boost::posix_time::from_time_t(rtklib_utc_time.time);
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p_time += boost::posix_time::microseconds(static_cast<long>(round(rtklib_utc_time.sec * 1e6)));
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this->set_position_UTC_time(p_time);
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cart2geo(static_cast<double>(rx_position_and_time(0)), static_cast<double>(rx_position_and_time(1)), static_cast<double>(rx_position_and_time(2)), 4);
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cart_to_geo(static_cast<double>(rx_position_and_time(0)), static_cast<double>(rx_position_and_time(1)), static_cast<double>(rx_position_and_time(2)), 4);
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DLOG(INFO) << "RTKLIB Position at " << boost::posix_time::to_simple_string(p_time)
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<< " is Lat = " << this->get_latitude() << " [deg], Long = " << this->get_longitude()
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