gnss-sdr/src/tests/unit-tests/signal-processing-blocks/observables/hybrid_observables_test.cc

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/*!
* \file hybrid_observables_test.cc
* \brief This class implements a tracking test for Galileo_E5a_DLL_PLL_Tracking
* implementation based on some input parameters.
* \author Javier Arribas, 2015. jarribas(at)cttc.es
*
*
* -------------------------------------------------------------------------
*
* Copyright (C) 2012-2015 (see AUTHORS file for a list of contributors)
*
* GNSS-SDR is a software defined Global Navigation
* Satellite Systems receiver
*
* This file is part of GNSS-SDR.
*
* GNSS-SDR is free software: you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation, either version 3 of the License, or
* (at your option) any later version.
*
* GNSS-SDR is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with GNSS-SDR. If not, see <http://www.gnu.org/licenses/>.
*
* -------------------------------------------------------------------------
*/
#include <unistd.h>
#include <chrono>
#include <exception>
#include <iostream>
#include <armadillo>
#include <gnuradio/top_block.h>
#include <gnuradio/blocks/file_source.h>
#include <gnuradio/analog/sig_source_waveform.h>
#include <gnuradio/analog/sig_source_c.h>
#include <gnuradio/blocks/interleaved_char_to_complex.h>
#include <gnuradio/blocks/null_sink.h>
#include <gnuradio/blocks/skiphead.h>
#include <gtest/gtest.h>
#include "GPS_L1_CA.h"
#include "gnss_satellite.h"
#include "gnss_block_factory.h"
#include "gnss_block_interface.h"
#include "tracking_interface.h"
#include "telemetry_decoder_interface.h"
#include "in_memory_configuration.h"
#include "gnss_synchro.h"
#include "gps_l1_ca_telemetry_decoder.h"
#include "tracking_true_obs_reader.h"
#include "true_observables_reader.h"
#include "tracking_dump_reader.h"
#include "observables_dump_reader.h"
#include "tlm_dump_reader.h"
#include "gps_l1_ca_dll_pll_tracking.h"
#include "gps_l1_ca_dll_pll_c_aid_tracking.h"
#include "hybrid_observables.h"
#include "signal_generator_flags.h"
// ######## GNURADIO BLOCK MESSAGE RECEVER FOR TRACKING MESSAGES #########
class HybridObservablesTest_msg_rx;
typedef boost::shared_ptr<HybridObservablesTest_msg_rx> HybridObservablesTest_msg_rx_sptr;
HybridObservablesTest_msg_rx_sptr HybridObservablesTest_msg_rx_make();
class HybridObservablesTest_msg_rx : public gr::block
{
private:
friend HybridObservablesTest_msg_rx_sptr HybridObservablesTest_msg_rx_make();
void msg_handler_events(pmt::pmt_t msg);
HybridObservablesTest_msg_rx();
public:
int rx_message;
~HybridObservablesTest_msg_rx(); //!< Default destructor
};
HybridObservablesTest_msg_rx_sptr HybridObservablesTest_msg_rx_make()
{
return HybridObservablesTest_msg_rx_sptr(new HybridObservablesTest_msg_rx());
}
void HybridObservablesTest_msg_rx::msg_handler_events(pmt::pmt_t msg)
{
try
{
long int message = pmt::to_long(msg);
rx_message = message;
}
catch(boost::bad_any_cast& e)
{
LOG(WARNING) << "msg_handler_telemetry Bad any cast!";
rx_message = 0;
}
}
HybridObservablesTest_msg_rx::HybridObservablesTest_msg_rx() :
gr::block("HybridObservablesTest_msg_rx", gr::io_signature::make(0, 0, 0), gr::io_signature::make(0, 0, 0))
{
this->message_port_register_in(pmt::mp("events"));
this->set_msg_handler(pmt::mp("events"), boost::bind(&HybridObservablesTest_msg_rx::msg_handler_events, this, _1));
rx_message = 0;
}
HybridObservablesTest_msg_rx::~HybridObservablesTest_msg_rx()
{}
// ###########################################################
// ######## GNURADIO BLOCK MESSAGE RECEVER FOR TLM MESSAGES #########
class HybridObservablesTest_tlm_msg_rx;
typedef boost::shared_ptr<HybridObservablesTest_tlm_msg_rx> HybridObservablesTest_tlm_msg_rx_sptr;
HybridObservablesTest_tlm_msg_rx_sptr HybridObservablesTest_tlm_msg_rx_make();
class HybridObservablesTest_tlm_msg_rx : public gr::block
{
private:
friend HybridObservablesTest_tlm_msg_rx_sptr HybridObservablesTest_tlm_msg_rx_make();
void msg_handler_events(pmt::pmt_t msg);
HybridObservablesTest_tlm_msg_rx();
public:
int rx_message;
~HybridObservablesTest_tlm_msg_rx(); //!< Default destructor
};
HybridObservablesTest_tlm_msg_rx_sptr HybridObservablesTest_tlm_msg_rx_make()
{
return HybridObservablesTest_tlm_msg_rx_sptr(new HybridObservablesTest_tlm_msg_rx());
}
void HybridObservablesTest_tlm_msg_rx::msg_handler_events(pmt::pmt_t msg)
{
try
{
long int message = pmt::to_long(msg);
rx_message = message;
}
catch(boost::bad_any_cast& e)
{
LOG(WARNING) << "msg_handler_telemetry Bad any cast!";
rx_message = 0;
}
}
HybridObservablesTest_tlm_msg_rx::HybridObservablesTest_tlm_msg_rx() :
gr::block("HybridObservablesTest_tlm_msg_rx", gr::io_signature::make(0, 0, 0), gr::io_signature::make(0, 0, 0))
{
this->message_port_register_in(pmt::mp("events"));
this->set_msg_handler(pmt::mp("events"), boost::bind(&HybridObservablesTest_tlm_msg_rx::msg_handler_events, this, _1));
rx_message = 0;
}
HybridObservablesTest_tlm_msg_rx::~HybridObservablesTest_tlm_msg_rx()
{}
// ###########################################################
class HybridObservablesTest: public ::testing::Test
{
public:
std::string generator_binary;
std::string p1;
std::string p2;
std::string p3;
std::string p4;
std::string p5;
const int baseband_sampling_freq = FLAGS_fs_gen_hz;
std::string filename_rinex_obs = FLAGS_filename_rinex_obs;
std::string filename_raw_data = FLAGS_filename_raw_data;
int configure_generator();
int generate_signal();
void check_results_carrier_phase(
arma::vec & true_ch0_phase_cycles,
arma::vec & true_ch1_phase_cycles,
arma::vec & true_ch0_tow_s,
arma::vec & measuded_ch0_phase_cycles,
arma::vec & measuded_ch1_phase_cycles,
arma::vec & measuded_ch0_RX_time_s);
void check_results_code_psudorange(
arma::vec & true_ch0_dist_m, arma::vec & true_ch1_dist_m,
arma::vec & true_ch0_tow_s,
arma::vec & measuded_ch0_Pseudorange_m,
arma::vec & measuded_ch1_Pseudorange_m,
arma::vec & measuded_ch0_RX_time_s);
HybridObservablesTest()
{
factory = std::make_shared<GNSSBlockFactory>();
config = std::make_shared<InMemoryConfiguration>();
item_size = sizeof(gr_complex);
gnss_synchro_ch0 = Gnss_Synchro();
gnss_synchro_ch1 = Gnss_Synchro();
}
~HybridObservablesTest()
{}
void configure_receiver();
gr::top_block_sptr top_block;
std::shared_ptr<GNSSBlockFactory> factory;
std::shared_ptr<InMemoryConfiguration> config;
Gnss_Synchro gnss_synchro_ch0;
Gnss_Synchro gnss_synchro_ch1;
size_t item_size;
};
int HybridObservablesTest::configure_generator()
{
// Configure signal generator
generator_binary = FLAGS_generator_binary;
p1 = std::string("-rinex_nav_file=") + FLAGS_rinex_nav_file;
if(FLAGS_dynamic_position.empty())
{
p2 = std::string("-static_position=") + FLAGS_static_position + std::string(",") + std::to_string(FLAGS_duration * 10);
}
else
{
p2 = std::string("-obs_pos_file=") + std::string(FLAGS_dynamic_position);
}
p3 = std::string("-rinex_obs_file=") + FLAGS_filename_rinex_obs; // RINEX 2.10 observation file output
p4 = std::string("-sig_out_file=") + FLAGS_filename_raw_data; // Baseband signal output file. Will be stored in int8_t IQ multiplexed samples
p5 = std::string("-sampling_freq=") + std::to_string(baseband_sampling_freq); //Baseband sampling frequency [MSps]
return 0;
}
int HybridObservablesTest::generate_signal()
{
int child_status;
char *const parmList[] = { &generator_binary[0], &generator_binary[0], &p1[0], &p2[0], &p3[0], &p4[0], &p5[0], NULL };
int pid;
if ((pid = fork()) == -1)
perror("fork err");
else if (pid == 0)
{
execv(&generator_binary[0], parmList);
std::cout << "Return not expected. Must be an execv err." << std::endl;
std::terminate();
}
waitpid(pid, &child_status, 0);
std::cout << "Signal and Observables RINEX and RAW files created." << std::endl;
return 0;
}
void HybridObservablesTest::configure_receiver()
{
gnss_synchro_ch0.Channel_ID = 0;
gnss_synchro_ch0.System = 'G';
std::string signal = "1C";
signal.copy(gnss_synchro_ch0.Signal, 2, 0);
gnss_synchro_ch0.PRN = FLAGS_test_satellite_PRN;
gnss_synchro_ch1.Channel_ID = 1;
gnss_synchro_ch1.System = 'G';
signal.copy(gnss_synchro_ch1.Signal, 2, 0);
gnss_synchro_ch1.PRN = FLAGS_test_satellite_PRN2;
config->set_property("GNSS-SDR.internal_fs_hz", std::to_string(baseband_sampling_freq));
// Set Tracking
config->set_property("Tracking_1C.item_type", "gr_complex");
config->set_property("Tracking_1C.if", "0");
config->set_property("Tracking_1C.dump", "true");
config->set_property("Tracking_1C.dump_filename", "./tracking_ch_");
config->set_property("Tracking_1C.pll_bw_hz", "15.0");
config->set_property("Tracking_1C.dll_bw_hz", "0.5");
config->set_property("Tracking_1C.early_late_space_chips", "0.5");
config->set_property("TelemetryDecoder_1C.dump","true");
config->set_property("Observables.dump","true");
}
void HybridObservablesTest::check_results_carrier_phase(
arma::vec & true_ch0_phase_cycles,
arma::vec & true_ch1_phase_cycles,
arma::vec & true_ch0_tow_s,
arma::vec & measuded_ch0_phase_cycles,
arma::vec & measuded_ch1_phase_cycles,
arma::vec & measuded_ch0_RX_time_s)
{
//1. True value interpolation to match the measurement times
arma::vec true_ch0_phase_interp;
arma::vec true_ch1_phase_interp;
arma::interp1(true_ch0_tow_s, true_ch0_phase_cycles, measuded_ch0_RX_time_s, true_ch0_phase_interp);
arma::interp1(true_ch0_tow_s, true_ch1_phase_cycles, measuded_ch0_RX_time_s, true_ch1_phase_interp);
//2. RMSE
arma::vec err_ch0_cycles;
arma::vec err_ch1_cycles;
//compute error without the accumulated carrier phase offsets (which depends on the receiver starting time)
err_ch0_cycles = measuded_ch0_phase_cycles - true_ch0_phase_interp - measuded_ch0_phase_cycles(0) + true_ch0_phase_interp(0);
err_ch1_cycles = measuded_ch1_phase_cycles - true_ch1_phase_interp - measuded_ch1_phase_cycles(0) + true_ch1_phase_interp(0);
arma::vec err2_ch0 = arma::square(err_ch0_cycles);
double rmse_ch0 = sqrt(arma::mean(err2_ch0));
//3. Mean err and variance
double error_mean_ch0 = arma::mean(err_ch0_cycles);
double error_var_ch0 = arma::var(err_ch0_cycles);
// 4. Peaks
double max_error_ch0 = arma::max(err_ch0_cycles);
double min_error_ch0 = arma::min(err_ch0_cycles);
arma::vec err2_ch1 = arma::square(err_ch1_cycles);
double rmse_ch1 = sqrt(arma::mean(err2_ch1));
//3. Mean err and variance
double error_mean_ch1 = arma::mean(err_ch1_cycles);
double error_var_ch1 = arma::var(err_ch1_cycles);
// 4. Peaks
double max_error_ch1 = arma::max(err_ch1_cycles);
double min_error_ch1 = arma::min(err_ch1_cycles);
//5. report
std::streamsize ss = std::cout.precision();
std::cout << std::setprecision(10) << "Channel 0 Carrier phase RMSE="
<< rmse_ch0 << ", mean=" << error_mean_ch0
<< ", stdev=" << sqrt(error_var_ch0)
<< " (max,min)=" << max_error_ch0
<< "," << min_error_ch0
<< " [cycles]" << std::endl;
std::cout.precision (ss);
ASSERT_LT(rmse_ch0, 1e-2);
ASSERT_LT(error_mean_ch0, 1e-2);
ASSERT_GT(error_mean_ch0, -1e-2);
ASSERT_LT(error_var_ch0, 1e-2);
ASSERT_LT(max_error_ch0, 5e-2);
ASSERT_GT(min_error_ch0, -5e-2);
//5. report
ss = std::cout.precision();
std::cout << std::setprecision(10) << "Channel 1 Carrier phase RMSE="
<< rmse_ch1 << ", mean=" << error_mean_ch1
<< ", stdev=" << sqrt(error_var_ch1)
<< " (max,min)=" << max_error_ch1
<< "," << min_error_ch1
<< " [cycles]" << std::endl;
std::cout.precision (ss);
ASSERT_LT(rmse_ch1, 1e-2);
ASSERT_LT(error_mean_ch1, 1e-2);
ASSERT_GT(error_mean_ch1, -1e-2);
ASSERT_LT(error_var_ch1, 1e-2);
ASSERT_LT(max_error_ch1, 5e-2);
ASSERT_GT(min_error_ch1, -5e-2);
}
void HybridObservablesTest::check_results_code_psudorange(
arma::vec & true_ch0_dist_m,
arma::vec & true_ch1_dist_m,
arma::vec & true_ch0_tow_s,
arma::vec & measuded_ch0_Pseudorange_m,
arma::vec & measuded_ch1_Pseudorange_m,
arma::vec & measuded_ch0_RX_time_s)
{
//1. True value interpolation to match the measurement times
arma::vec true_ch0_dist_interp;
arma::vec true_ch1_dist_interp;
arma::interp1(true_ch0_tow_s, true_ch0_dist_m, measuded_ch0_RX_time_s, true_ch0_dist_interp);
arma::interp1(true_ch0_tow_s, true_ch1_dist_m, measuded_ch0_RX_time_s, true_ch1_dist_interp);
// generate delta pseudoranges
arma::vec delta_true_dist_m = true_ch0_dist_interp-true_ch1_dist_interp;
arma::vec delta_measured_dist_m = measuded_ch0_Pseudorange_m-measuded_ch1_Pseudorange_m;
//2. RMSE
arma::vec err;
err = delta_measured_dist_m - delta_true_dist_m;
arma::vec err2 = arma::square(err);
double rmse = sqrt(arma::mean(err2));
//3. Mean err and variance
double error_mean = arma::mean(err);
double error_var = arma::var(err);
// 4. Peaks
double max_error = arma::max(err);
double min_error = arma::min(err);
//5. report
std::streamsize ss = std::cout.precision();
std::cout << std::setprecision(10) << "Delta Observables RMSE="
<< rmse << ", mean=" << error_mean
<< ", stdev=" << sqrt(error_var)
<< " (max,min)=" << max_error
<< "," << min_error
<< " [meters]" << std::endl;
std::cout.precision (ss);
ASSERT_LT(rmse, 0.5);
ASSERT_LT(error_mean, 0.5);
ASSERT_GT(error_mean, -0.5);
ASSERT_LT(error_var, 0.5);
ASSERT_LT(max_error, 2);
ASSERT_GT(min_error, -2);
}
TEST_F(HybridObservablesTest, ValidationOfResults)
{
// Configure the signal generator
configure_generator();
// Generate signal raw signal samples and observations RINEX file
if (FLAGS_disable_generator==false)
{
generate_signal();
}
std::chrono::time_point<std::chrono::system_clock> start, end;
std::chrono::duration<double> elapsed_seconds(0);
configure_receiver();
//open true observables log file written by the simulator
tracking_true_obs_reader true_obs_data_ch0;
tracking_true_obs_reader true_obs_data_ch1;
int test_satellite_PRN = FLAGS_test_satellite_PRN;
int test_satellite_PRN2 = FLAGS_test_satellite_PRN2;
std::cout << "Testing satellite PRNs " << test_satellite_PRN <<","<<test_satellite_PRN << std::endl;
std::string true_obs_file = std::string("./gps_l1_ca_obs_prn");
true_obs_file.append(std::to_string(test_satellite_PRN));
true_obs_file.append(".dat");
ASSERT_NO_THROW({
if (true_obs_data_ch0.open_obs_file(true_obs_file) == false)
{
throw std::exception();
};
}) << "Failure opening true observables file" << std::endl;
true_obs_file = std::string("./gps_l1_ca_obs_prn");
true_obs_file.append(std::to_string(test_satellite_PRN2));
true_obs_file.append(".dat");
ASSERT_NO_THROW({
if (true_obs_data_ch1.open_obs_file(true_obs_file) == false)
{
throw std::exception();
};
}) << "Failure opening true observables file" << std::endl;
top_block = gr::make_top_block("Telemetry_Decoder test");
std::shared_ptr<TrackingInterface> tracking_ch0 = std::make_shared<GpsL1CaDllPllTracking>(config.get(), "Tracking_1C", 1, 1);
//std::shared_ptr<TrackingInterface> tracking_ch1 = std::make_shared<GpsL1CaDllPllCAidTracking>(config.get(), "Tracking_1C", 1, 1);
std::shared_ptr<TrackingInterface> tracking_ch1 = std::make_shared<GpsL1CaDllPllTracking>(config.get(), "Tracking_1C", 1, 1);
//std::shared_ptr<TrackingInterface> tracking_ch1 = std::make_shared<GpsL1CaDllPllCAidTracking>(config.get(), "Tracking_1C", 1, 1);
boost::shared_ptr<HybridObservablesTest_msg_rx> msg_rx_ch0 = HybridObservablesTest_msg_rx_make();
boost::shared_ptr<HybridObservablesTest_msg_rx> msg_rx_ch1 = HybridObservablesTest_msg_rx_make();
// load acquisition data based on the first epoch of the true observations
ASSERT_NO_THROW({
if (true_obs_data_ch0.read_binary_obs() == false)
{
throw std::exception();
};
})<< "Failure reading true observables file" << std::endl;
ASSERT_NO_THROW({
if (true_obs_data_ch1.read_binary_obs() == false)
{
throw std::exception();
};
}) << "Failure reading true observables file" << std::endl;
//restart the epoch counter
true_obs_data_ch0.restart();
true_obs_data_ch1.restart();
std::cout << "Initial Doppler [Hz]=" << true_obs_data_ch0.doppler_l1_hz << " Initial code delay [Chips]=" << true_obs_data_ch0.prn_delay_chips << std::endl;
gnss_synchro_ch0.Acq_delay_samples = (GPS_L1_CA_CODE_LENGTH_CHIPS - true_obs_data_ch0.prn_delay_chips / GPS_L1_CA_CODE_LENGTH_CHIPS) * baseband_sampling_freq * GPS_L1_CA_CODE_PERIOD;
gnss_synchro_ch0.Acq_doppler_hz = true_obs_data_ch0.doppler_l1_hz;
gnss_synchro_ch0.Acq_samplestamp_samples = 0;
std::cout << "Initial Doppler [Hz]=" << true_obs_data_ch1.doppler_l1_hz << " Initial code delay [Chips]=" << true_obs_data_ch1.prn_delay_chips << std::endl;
gnss_synchro_ch1.Acq_delay_samples = (GPS_L1_CA_CODE_LENGTH_CHIPS - true_obs_data_ch1.prn_delay_chips / GPS_L1_CA_CODE_LENGTH_CHIPS) * baseband_sampling_freq * GPS_L1_CA_CODE_PERIOD;
gnss_synchro_ch1.Acq_doppler_hz = true_obs_data_ch1.doppler_l1_hz;
gnss_synchro_ch1.Acq_samplestamp_samples = 0;
//telemetry decoders
std::shared_ptr<TelemetryDecoderInterface> tlm_ch0(new GpsL1CaTelemetryDecoder(config.get(), "TelemetryDecoder_1C",1, 1));
std::shared_ptr<TelemetryDecoderInterface> tlm_ch1(new GpsL1CaTelemetryDecoder(config.get(), "TelemetryDecoder_1C",1, 1));
ASSERT_NO_THROW( {
tlm_ch0->set_channel(0);
tlm_ch1->set_channel(1);
tlm_ch0->set_satellite(Gnss_Satellite(std::string("GPS"),gnss_synchro_ch0.PRN));
tlm_ch1->set_satellite(Gnss_Satellite(std::string("GPS"),gnss_synchro_ch1.PRN));
}) << "Failure setting gnss_synchro." << std::endl;
boost::shared_ptr<HybridObservablesTest_tlm_msg_rx> tlm_msg_rx_ch1 = HybridObservablesTest_tlm_msg_rx_make();
boost::shared_ptr<HybridObservablesTest_tlm_msg_rx> tlm_msg_rx_ch2 = HybridObservablesTest_tlm_msg_rx_make();
//Observables
std::shared_ptr<ObservablesInterface> observables(new HybridObservables(config.get(), "Observables",2, 2));
ASSERT_NO_THROW( {
tracking_ch0->set_channel(gnss_synchro_ch0.Channel_ID);
tracking_ch1->set_channel(gnss_synchro_ch1.Channel_ID);
}) << "Failure setting channel." << std::endl;
ASSERT_NO_THROW( {
tracking_ch0->set_gnss_synchro(&gnss_synchro_ch0);
tracking_ch1->set_gnss_synchro(&gnss_synchro_ch1);
}) << "Failure setting gnss_synchro." << std::endl;
ASSERT_NO_THROW( {
tracking_ch0->connect(top_block);
tracking_ch1->connect(top_block);
}) << "Failure connecting tracking to the top_block." << std::endl;
ASSERT_NO_THROW( {
std::string file = "./" + filename_raw_data;
const char * file_name = file.c_str();
gr::blocks::file_source::sptr file_source = gr::blocks::file_source::make(sizeof(int8_t), file_name, false);
gr::blocks::interleaved_char_to_complex::sptr gr_interleaved_char_to_complex = gr::blocks::interleaved_char_to_complex::make();
gr::blocks::null_sink::sptr sink_ch0 = gr::blocks::null_sink::make(sizeof(Gnss_Synchro));
gr::blocks::null_sink::sptr sink_ch1 = gr::blocks::null_sink::make(sizeof(Gnss_Synchro));
top_block->connect(file_source, 0, gr_interleaved_char_to_complex, 0);
//ch0
top_block->connect(gr_interleaved_char_to_complex, 0, tracking_ch0->get_left_block(), 0);
top_block->connect(tracking_ch0->get_right_block(), 0, tlm_ch0->get_left_block(), 0);
top_block->connect(tlm_ch0->get_right_block(), 0, observables->get_left_block(), 0);
top_block->msg_connect(tracking_ch0->get_right_block(), pmt::mp("events"), msg_rx_ch0, pmt::mp("events"));
//ch1
top_block->connect(gr_interleaved_char_to_complex, 0, tracking_ch1->get_left_block(), 0);
top_block->connect(tracking_ch1->get_right_block(), 0, tlm_ch1->get_left_block(), 0);
top_block->connect(tlm_ch1->get_right_block(), 0, observables->get_left_block(), 1);
top_block->msg_connect(tracking_ch1->get_right_block(), pmt::mp("events"), msg_rx_ch1, pmt::mp("events"));
top_block->connect(observables->get_right_block(), 0, sink_ch0, 0);
top_block->connect(observables->get_right_block(), 1, sink_ch1, 0);
}) << "Failure connecting the blocks." << std::endl;
tracking_ch0->start_tracking();
tracking_ch1->start_tracking();
EXPECT_NO_THROW( {
start = std::chrono::system_clock::now();
top_block->run(); // Start threads and wait
end = std::chrono::system_clock::now();
elapsed_seconds = end - start;
}) << "Failure running the top_block." << std::endl;
//check results
//load the true values
true_observables_reader true_observables;
ASSERT_NO_THROW({
if ( true_observables.open_obs_file(std::string("./obs_out.bin")) == false)
{
throw std::exception();
};
}) << "Failure opening true observables file" << std::endl;
long int nepoch = true_observables.num_epochs();
std::cout << "True observation epochs=" << nepoch << std::endl;
arma::vec true_ch0_dist_m = arma::zeros(nepoch, 1);
arma::vec true_ch0_acc_carrier_phase_cycles = arma::zeros(nepoch, 1);
arma::vec true_ch0_Doppler_Hz = arma::zeros(nepoch, 1);
arma::vec true_ch0_tow_s = arma::zeros(nepoch, 1);
arma::vec true_ch1_dist_m = arma::zeros(nepoch, 1);
arma::vec true_ch1_acc_carrier_phase_cycles = arma::zeros(nepoch, 1);
arma::vec true_ch1_Doppler_Hz = arma::zeros(nepoch, 1);
arma::vec true_ch1_tow_s = arma::zeros(nepoch, 1);
true_observables.restart();
long int epoch_counter = 0;
ASSERT_NO_THROW({
while(true_observables.read_binary_obs())
{
if (round(true_observables.prn[0])!=gnss_synchro_ch0.PRN)
{
std::cout<<"True observables SV PRN do not match"<<round(true_observables.prn[1])<<std::endl;
throw std::exception();
}
if (round(true_observables.prn[1])!=gnss_synchro_ch1.PRN)
{
std::cout<<"True observables SV PRN do not match "<<round(true_observables.prn[1])<<std::endl;
throw std::exception();
}
true_ch0_tow_s(epoch_counter) = true_observables.gps_time_sec[0];
true_ch0_dist_m(epoch_counter) = true_observables.dist_m[0];
true_ch0_Doppler_Hz(epoch_counter) = true_observables.doppler_l1_hz[0];
true_ch0_acc_carrier_phase_cycles(epoch_counter) = true_observables.acc_carrier_phase_l1_cycles[0];
true_ch1_tow_s(epoch_counter) = true_observables.gps_time_sec[1];
true_ch1_dist_m(epoch_counter) = true_observables.dist_m[1];
true_ch1_Doppler_Hz(epoch_counter) = true_observables.doppler_l1_hz[1];
true_ch1_acc_carrier_phase_cycles(epoch_counter) = true_observables.acc_carrier_phase_l1_cycles[1];
epoch_counter++;
}
});
//read measured values
observables_dump_reader estimated_observables(2); //two channels
ASSERT_NO_THROW({
if (estimated_observables.open_obs_file(std::string("./observables.dat")) == false)
{
throw std::exception();
};
}) << "Failure opening dump observables file" << std::endl;
nepoch = estimated_observables.num_epochs();
std::cout << "Measured observation epochs=" << nepoch << std::endl;
arma::vec measuded_ch0_RX_time_s = arma::zeros(nepoch, 1);
arma::vec measuded_ch0_TOW_at_current_symbol_s = arma::zeros(nepoch, 1);
arma::vec measuded_ch0_Carrier_Doppler_hz = arma::zeros(nepoch, 1);
arma::vec measuded_ch0_Acc_carrier_phase_hz = arma::zeros(nepoch, 1);
arma::vec measuded_ch0_Pseudorange_m = arma::zeros(nepoch, 1);
arma::vec measuded_ch1_RX_time_s = arma::zeros(nepoch, 1);
arma::vec measuded_ch1_TOW_at_current_symbol_s = arma::zeros(nepoch, 1);
arma::vec measuded_ch1_Carrier_Doppler_hz = arma::zeros(nepoch, 1);
arma::vec measuded_ch1_Acc_carrier_phase_hz = arma::zeros(nepoch, 1);
arma::vec measuded_ch1_Pseudorange_m = arma::zeros(nepoch, 1);
estimated_observables.restart();
epoch_counter = 0;
while(estimated_observables.read_binary_obs())
{
measuded_ch0_RX_time_s(epoch_counter) = estimated_observables.RX_time[0];
measuded_ch0_TOW_at_current_symbol_s(epoch_counter) =estimated_observables.TOW_at_current_symbol_s[0];
measuded_ch0_Carrier_Doppler_hz(epoch_counter) = estimated_observables.Carrier_Doppler_hz[0];
measuded_ch0_Acc_carrier_phase_hz(epoch_counter) = estimated_observables.Acc_carrier_phase_hz[0];
measuded_ch0_Pseudorange_m(epoch_counter) = estimated_observables.Pseudorange_m[0];
measuded_ch1_RX_time_s(epoch_counter) = estimated_observables.RX_time[1];
measuded_ch1_TOW_at_current_symbol_s(epoch_counter) =estimated_observables.TOW_at_current_symbol_s[1];
measuded_ch1_Carrier_Doppler_hz(epoch_counter) = estimated_observables.Carrier_Doppler_hz[1];
measuded_ch1_Acc_carrier_phase_hz(epoch_counter) = estimated_observables.Acc_carrier_phase_hz[1];
measuded_ch1_Pseudorange_m(epoch_counter) = estimated_observables.Pseudorange_m[1];
epoch_counter++;
}
//Cut measurement initial transitory of the measurements
arma::uvec initial_meas_point = arma::find(measuded_ch0_RX_time_s >= true_ch0_tow_s(0), 1, "first");
measuded_ch0_RX_time_s = measuded_ch0_RX_time_s.subvec(initial_meas_point(0), measuded_ch0_RX_time_s.size() - 1);
measuded_ch0_Pseudorange_m = measuded_ch0_Pseudorange_m.subvec(initial_meas_point(0), measuded_ch0_Pseudorange_m.size() - 1);
measuded_ch0_Acc_carrier_phase_hz = measuded_ch0_Acc_carrier_phase_hz.subvec(initial_meas_point(0), measuded_ch0_Acc_carrier_phase_hz.size() - 1);
measuded_ch1_RX_time_s = measuded_ch1_RX_time_s.subvec(initial_meas_point(0), measuded_ch1_RX_time_s.size() - 1);
measuded_ch1_Pseudorange_m = measuded_ch1_Pseudorange_m.subvec(initial_meas_point(0), measuded_ch1_Pseudorange_m.size() - 1);
measuded_ch1_Acc_carrier_phase_hz = measuded_ch1_Acc_carrier_phase_hz.subvec(initial_meas_point(0), measuded_ch1_Acc_carrier_phase_hz.size() - 1);
//correct the clock error using true values (it is not possible for a receiver to correct
//the receiver clock offset error at the observables level because it is required the
//decoding of the ephemeris data and solve the PVT equations)
//find the reference satellite and compute the receiver time offset at obsevable level
arma::vec receiver_time_offset_s;
if (measuded_ch0_Pseudorange_m(0)<measuded_ch1_Pseudorange_m(0))
{
receiver_time_offset_s = true_ch0_dist_m / GPS_C_m_s - GPS_STARTOFFSET_ms/1000.0;
}
else
{
receiver_time_offset_s = true_ch1_dist_m / GPS_C_m_s - GPS_STARTOFFSET_ms/1000.0;
}
arma::vec corrected_reference_TOW_s = true_ch0_tow_s - receiver_time_offset_s;
std::cout <<" receiver_time_offset_s [0]: " << receiver_time_offset_s(0) << std::endl;
//compare measured observables
check_results_code_psudorange(true_ch0_dist_m, true_ch1_dist_m, corrected_reference_TOW_s,
measuded_ch0_Pseudorange_m,measuded_ch1_Pseudorange_m, measuded_ch0_RX_time_s);
check_results_carrier_phase(true_ch0_acc_carrier_phase_cycles,
true_ch1_acc_carrier_phase_cycles,
corrected_reference_TOW_s,
measuded_ch0_Acc_carrier_phase_hz,
measuded_ch1_Acc_carrier_phase_hz,
measuded_ch0_RX_time_s);
std::cout << "Test completed in " << elapsed_seconds.count() * 1e6 << " microseconds" << std::endl;
}