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https://github.com/gnss-sdr/gnss-sdr
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385 lines
17 KiB
C++
385 lines
17 KiB
C++
/*!
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* \file front_end_cal.cc
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* \brief Implementation of the Front-end calibration program.
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* \author Javier Arribas, 2013. jarribas(at)cttc.es
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*
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*
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* -----------------------------------------------------------------------------
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*
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* GNSS-SDR is a Global Navigation Satellite System software-defined receiver.
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* This file is part of GNSS-SDR.
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*
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* Copyright (C) 2010-2020 (see AUTHORS file for a list of contributors)
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* SPDX-License-Identifier: GPL-3.0-or-later
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*
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* -----------------------------------------------------------------------------
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*/
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#include "front_end_cal.h"
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#include "GPS_L1_CA.h" // for GPS_L1_FREQ_HZ
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#include "concurrent_map.h"
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#include "configuration_interface.h"
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#include "gnss_sdr_supl_client.h"
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#include "gps_acq_assist.h" // for Gps_Acq_Assist
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#include "gps_almanac.h"
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#include "gps_ephemeris.h"
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#include "gps_iono.h"
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#include "gps_utc_model.h"
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#include <boost/lexical_cast.hpp>
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#include <algorithm> // for min
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#include <cmath>
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#include <iostream> // for operator<<
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#include <map>
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#include <stdexcept>
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#include <utility>
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#if USE_GLOG_AND_GFLAGS
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#include <glog/logging.h>
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#else
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#include <absl/log/log.h>
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#endif
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extern Concurrent_Map<Gps_Ephemeris> global_gps_ephemeris_map;
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extern Concurrent_Map<Gps_Iono> global_gps_iono_map;
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extern Concurrent_Map<Gps_Utc_Model> global_gps_utc_model_map;
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extern Concurrent_Map<Gps_Almanac> global_gps_almanac_map;
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extern Concurrent_Map<Gps_Acq_Assist> global_gps_acq_assist_map;
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bool FrontEndCal::read_assistance_from_XML()
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{
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Gnss_Sdr_Supl_Client supl_client_ephemeris_;
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std::string eph_xml_filename = "gps_ephemeris.xml";
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std::cout << "SUPL: Trying to read GPS ephemeris from XML file " << eph_xml_filename << '\n';
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LOG(INFO) << "SUPL: Trying to read GPS ephemeris from XML file " << eph_xml_filename;
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if (supl_client_ephemeris_.load_ephemeris_xml(eph_xml_filename) == true)
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{
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std::map<int, Gps_Ephemeris>::iterator gps_eph_iter;
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for (gps_eph_iter = supl_client_ephemeris_.gps_ephemeris_map.begin();
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gps_eph_iter != supl_client_ephemeris_.gps_ephemeris_map.end();
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gps_eph_iter++)
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{
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std::cout << "SUPL: Read XML Ephemeris for GPS SV " << gps_eph_iter->first << '\n';
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LOG(INFO) << "SUPL: Read XML Ephemeris for GPS SV " << gps_eph_iter->first;
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LOG(INFO) << "New Ephemeris record inserted with Toe=" << gps_eph_iter->second.toe << " and GPS Week=" << gps_eph_iter->second.WN;
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global_gps_ephemeris_map.write(gps_eph_iter->second.PRN, gps_eph_iter->second);
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}
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return true;
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}
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std::cout << "ERROR: SUPL client error reading XML\n";
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LOG(WARNING) << "ERROR: SUPL client error reading XML";
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return false;
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}
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int FrontEndCal::Get_SUPL_Assist()
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{
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// ######### GNSS Assistance #################################
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Gnss_Sdr_Supl_Client supl_client_acquisition_;
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Gnss_Sdr_Supl_Client supl_client_ephemeris_;
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int supl_mcc; // Current network MCC (Mobile country code), 3 digits.
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int supl_mns; // Current network MNC (Mobile Network code), 2 or 3 digits.
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int supl_lac; // Current network LAC (Location area code),16 bits, 1-65520 are valid values.
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int supl_ci; // Cell Identity (16 bits, 0-65535 are valid values).
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// GNSS Assistance configuration
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int error = 0;
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bool enable_gps_supl_assistance = configuration_->property("GNSS-SDR.SUPL_gps_enabled", false);
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if (enable_gps_supl_assistance == true)
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// SUPL SERVER TEST. Not operational yet!
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{
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LOG(INFO) << "SUPL RRLP GPS assistance enabled!";
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std::string default_acq_server = "supl.nokia.com";
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std::string default_eph_server = "supl.google.com";
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supl_client_ephemeris_.server_name = configuration_->property("GNSS-SDR.SUPL_gps_ephemeris_server", std::move(default_acq_server));
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supl_client_acquisition_.server_name = configuration_->property("GNSS-SDR.SUPL_gps_acquisition_server", std::move(default_eph_server));
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supl_client_ephemeris_.server_port = configuration_->property("GNSS-SDR.SUPL_gps_ephemeris_port", 7275);
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supl_client_acquisition_.server_port = configuration_->property("GNSS-SDR.SUPL_gps_acquisition_port", 7275);
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supl_mcc = configuration_->property("GNSS-SDR.SUPL_MCC", 244);
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supl_mns = configuration_->property("GNSS-SDR.SUPL_MNC", 5);
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std::string default_lac = "0x59e2";
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std::string default_ci = "0x31b0";
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try
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{
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supl_lac = boost::lexical_cast<int>(configuration_->property("GNSS-SDR.SUPL_LAC", std::move(default_lac)));
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}
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catch (boost::bad_lexical_cast &)
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{
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supl_lac = 0x59e2;
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}
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try
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{
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supl_ci = boost::lexical_cast<int>(configuration_->property("GNSS-SDR.SUPL_CI", std::move(default_ci)));
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}
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catch (boost::bad_lexical_cast &)
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{
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supl_ci = 0x31b0;
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}
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bool SUPL_read_gps_assistance_xml = configuration_->property("GNSS-SDR.SUPL_read_gps_assistance_xml", false);
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if (SUPL_read_gps_assistance_xml == true)
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{
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// read assistance from file
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read_assistance_from_XML();
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}
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else
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{
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// Request ephemeris from SUPL server
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supl_client_ephemeris_.request = 1;
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LOG(INFO) << "SUPL: Trying to read GPS ephemeris from SUPL server...";
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std::cout << "SUPL: Trying to read GPS ephemeris from SUPL server...\n";
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error = supl_client_ephemeris_.get_assistance(supl_mcc, supl_mns, supl_lac, supl_ci);
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if (error == 0)
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{
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std::map<int, Gps_Ephemeris>::iterator gps_eph_iter;
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for (gps_eph_iter = supl_client_ephemeris_.gps_ephemeris_map.begin();
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gps_eph_iter != supl_client_ephemeris_.gps_ephemeris_map.end();
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gps_eph_iter++)
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{
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LOG(INFO) << "SUPL: Received Ephemeris for GPS SV " << gps_eph_iter->first;
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std::cout << "SUPL: Received Ephemeris for GPS SV " << gps_eph_iter->first << '\n';
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LOG(INFO) << "New Ephemeris record inserted with Toe=" << gps_eph_iter->second.toe << " and GPS Week=" << gps_eph_iter->second.WN;
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global_gps_ephemeris_map.write(gps_eph_iter->second.PRN, gps_eph_iter->second);
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}
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// Save ephemeris to XML file
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std::string eph_xml_filename = configuration_->property("GNSS-SDR.SUPL_gps_ephemeris_xml", eph_default_xml_filename);
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if (supl_client_ephemeris_.save_ephemeris_map_xml(eph_xml_filename, supl_client_ephemeris_.gps_ephemeris_map) == true)
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{
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LOG(INFO) << "SUPL: XML Ephemeris file created.";
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}
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}
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else
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{
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LOG(WARNING) << "ERROR: SUPL client for Ephemeris returned " << error;
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std::cout << "ERROR in SUPL client. Please check your Internet connection and SUPL server configuration\n";
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}
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// Request almanac , IONO and UTC Model
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supl_client_ephemeris_.request = 0;
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LOG(INFO) << "SUPL: Try read Almanac, Iono, Utc Model, Ref Time and Ref Location from SUPL server...";
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error = supl_client_ephemeris_.get_assistance(supl_mcc, supl_mns, supl_lac, supl_ci);
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if (error == 0)
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{
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std::map<int, Gps_Almanac>::iterator gps_alm_iter;
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for (gps_alm_iter = supl_client_ephemeris_.gps_almanac_map.begin();
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gps_alm_iter != supl_client_ephemeris_.gps_almanac_map.end();
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gps_alm_iter++)
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{
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LOG(INFO) << "SUPL: Received Almanac for GPS SV " << gps_alm_iter->first;
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std::cout << "SUPL: Received Almanac for GPS SV " << gps_alm_iter->first << '\n';
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global_gps_almanac_map.write(gps_alm_iter->first, gps_alm_iter->second);
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}
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if (supl_client_ephemeris_.gps_iono.valid == true)
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{
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LOG(INFO) << "SUPL: Received GPS Iono";
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std::cout << "SUPL: Received GPS Iono\n";
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global_gps_iono_map.write(0, supl_client_ephemeris_.gps_iono);
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}
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if (supl_client_ephemeris_.gps_utc.valid == true)
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{
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LOG(INFO) << "SUPL: Received GPS UTC Model";
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std::cout << "SUPL: Received GPS UTC Model\n";
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global_gps_utc_model_map.write(0, supl_client_ephemeris_.gps_utc);
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}
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}
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else
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{
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LOG(WARNING) << "ERROR: SUPL client for Almanac returned " << error;
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std::cout << "ERROR in SUPL client. Please check your Internet connection and SUPL server configuration\n";
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}
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// Request acquisition assistance
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supl_client_acquisition_.request = 2;
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LOG(INFO) << "SUPL: Trying to read Acquisition assistance from SUPL server...";
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std::cout << "SUPL: Trying to read Acquisition assistance from SUPL server...\n";
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error = supl_client_acquisition_.get_assistance(supl_mcc, supl_mns, supl_lac, supl_ci);
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if (error == 0)
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{
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std::map<int, Gps_Acq_Assist>::iterator gps_acq_iter;
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for (gps_acq_iter = supl_client_acquisition_.gps_acq_map.begin();
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gps_acq_iter != supl_client_acquisition_.gps_acq_map.end();
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gps_acq_iter++)
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{
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LOG(INFO) << "SUPL: Received Acquisition assistance for GPS SV " << gps_acq_iter->first;
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std::cout << "SUPL: Received Acquisition assistance for GPS SV " << gps_acq_iter->first << '\n';
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LOG(INFO) << "New acq assist record inserted";
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global_gps_acq_assist_map.write(gps_acq_iter->second.PRN, gps_acq_iter->second);
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}
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}
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else
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{
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LOG(WARNING) << "ERROR: SUPL client for Acquisition assistance returned " << error;
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std::cout << "ERROR in SUPL client. Please check your Internet connection and SUPL server configuration\n";
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}
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}
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}
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return error;
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}
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void FrontEndCal::set_configuration(std::shared_ptr<ConfigurationInterface> configuration)
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{
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configuration_ = std::move(configuration);
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}
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bool FrontEndCal::get_ephemeris()
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{
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bool read_ephemeris_from_xml = configuration_->property("GNSS-SDR.read_eph_from_xml", false);
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if (read_ephemeris_from_xml == true)
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{
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std::cout << "Trying to read ephemeris from XML file...\n";
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LOG(INFO) << "Trying to read ephemeris from XML file...";
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if (read_assistance_from_XML() == false)
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{
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std::cout << "ERROR: Could not read Ephemeris file: Trying to get ephemeris from SUPL server...\n";
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LOG(INFO) << "ERROR: Could not read Ephemeris file: Trying to get ephemeris from SUPL server...";
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if (Get_SUPL_Assist() == 1)
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{
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return true;
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}
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return false;
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}
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return true;
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}
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std::cout << "Trying to read ephemeris from SUPL server...\n";
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LOG(INFO) << "Trying to read ephemeris from SUPL server...";
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if (Get_SUPL_Assist() == 0)
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{
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return true;
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}
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return false;
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}
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arma::vec FrontEndCal::lla2ecef(const arma::vec &lla)
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{
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// WGS84 flattening
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double f = 1.0 / 298.257223563;
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// WGS84 equatorial radius
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double R = 6378137.0;
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arma::vec ellipsoid = "0.0 0.0";
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double phi = (lla(0) / 360.0) * TWO_PI;
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double lambda = (lla(1) / 360.0) * TWO_PI;
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ellipsoid(0) = R;
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ellipsoid(1) = sqrt(1.0 - (1.0 - f) * (1.0 - f));
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arma::vec ecef = "0.0 0.0 0.0 0.0";
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ecef = geodetic2ecef(phi, lambda, lla(3), ellipsoid);
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return ecef;
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}
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arma::vec FrontEndCal::geodetic2ecef(double phi, double lambda, double h, const arma::vec &ellipsoid)
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{
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double a = ellipsoid(0);
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double e2 = ellipsoid(1) * ellipsoid(1);
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double sinphi = sin(phi);
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double cosphi = cos(phi);
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double N = a / sqrt(1.0 - e2 * sinphi * sinphi);
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arma::vec ecef = "0.0 0.0 0.0 0.0";
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ecef(0) = (N + h) * cosphi * cos(lambda);
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ecef(1) = (N + h) * cosphi * sin(lambda);
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ecef(2) = (N * (1.0 - e2) + h) * sinphi;
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return ecef;
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}
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double FrontEndCal::estimate_doppler_from_eph(unsigned int PRN, double tow, double lat, double lon, double height) noexcept(false)
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{
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int num_secs = 10;
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double step_secs = 0.5;
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// Observer position ECEF
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arma::vec obs_ecef = "0.0 0.0 0.0 0.0";
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arma::vec lla = "0.0 0.0 0.0 0.0";
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lla(0) = lat;
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lla(1) = lon;
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lla(2) = height;
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obs_ecef = lla2ecef(lla);
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// Satellite positions ECEF
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std::map<int, Gps_Ephemeris> eph_map;
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eph_map = global_gps_ephemeris_map.get_map_copy();
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std::map<int, Gps_Ephemeris>::iterator eph_it;
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eph_it = eph_map.find(PRN);
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if (eph_it != eph_map.end())
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{
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arma::vec SV_pos_ecef = "0.0 0.0 0.0 0.0";
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double obs_time_start;
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double obs_time_stop;
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obs_time_start = tow - static_cast<double>(num_secs) / 2.0;
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obs_time_stop = tow + static_cast<double>(num_secs) / 2.0;
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int n_points = round((obs_time_stop - obs_time_start) / step_secs);
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arma::vec ranges = arma::zeros(n_points, 1);
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double obs_time = obs_time_start;
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for (int i = 0; i < n_points; i++)
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{
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eph_it->second.satellitePosition(obs_time);
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SV_pos_ecef(0) = eph_it->second.satpos_X;
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SV_pos_ecef(1) = eph_it->second.satpos_Y;
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SV_pos_ecef(2) = eph_it->second.satpos_Z;
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// SV distances to observer (true range)
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ranges(i) = arma::norm(SV_pos_ecef - obs_ecef, 2);
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obs_time += step_secs;
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}
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// Observer to satellite radial velocity
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// Numeric derivative: Positive slope means that the distance from obs to
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// satellite is increasing
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arma::vec obs_to_sat_velocity;
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obs_to_sat_velocity = (ranges.subvec(1, (n_points - 1)) - ranges.subvec(0, (n_points - 2))) / step_secs;
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// Doppler equations are formulated accounting for positive velocities if the
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// tx and rx are approaching to each other. So, the satellite velocity must
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// be redefined as:
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obs_to_sat_velocity = -obs_to_sat_velocity;
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// Doppler estimation
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arma::vec Doppler_Hz;
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Doppler_Hz = (obs_to_sat_velocity / SPEED_OF_LIGHT_M_S) * GPS_L1_FREQ_HZ;
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double mean_Doppler_Hz;
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mean_Doppler_Hz = arma::mean(Doppler_Hz);
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return mean_Doppler_Hz;
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}
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throw std::runtime_error("1");
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}
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void FrontEndCal::GPS_L1_front_end_model_E4000(double f_bb_true_Hz, double f_bb_meas_Hz, double fs_nominal_hz, double *estimated_fs_Hz, double *estimated_f_if_Hz, double *f_osc_err_ppm)
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{
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const double f_osc_n = 28.8e6;
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// PLL registers settings (according to E4000 datasheet)
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const double N = 109.0;
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const double Y = 65536.0;
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const double X = 26487.0;
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const double R = 2.0;
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// Obtained RF center frequency
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double f_rf_pll = (f_osc_n * (N + X / Y)) / R;
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// RF frequency error caused by fractional PLL roundings
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double f_bb_err_pll = GPS_L1_FREQ_HZ - f_rf_pll;
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// Measured F_rf error
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double f_rf_err = (f_bb_meas_Hz - f_bb_true_Hz) - f_bb_err_pll;
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double f_osc_err_hz = (f_rf_err * R) / (N + X / Y);
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f_osc_err_hz = -f_osc_err_hz;
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*f_osc_err_ppm = f_osc_err_hz / (f_osc_n / 1e6);
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double frac = fs_nominal_hz / f_osc_n;
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*estimated_fs_Hz = frac * (f_osc_n + f_osc_err_hz);
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*estimated_f_if_Hz = f_rf_err;
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}
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