mirror of https://github.com/gnss-sdr/gnss-sdr
PVT block enabled to find ephemeris and observables from both GPS and Galileo
This commit is contained in:
marabra
parent
25934c477e
commit
e7c4b35238
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@ -152,7 +152,7 @@ int hybrid_pvt_cc::general_work (int noutput_items, gr_vector_int &ninput_items,
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//d_rx_time = in[i][0].d_TOW_at_current_symbol; // all the channels have the same RX timestamp (common RX time pseudoranges)
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d_TOW_at_curr_symbol_constellation=in[i][0].d_TOW_at_current_symbol; // d_TOW_at_current_symbol not corrected by delta t (just for debug)
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d_rx_time = in[i][0].d_TOW_hybrid_at_current_symbol; // hybrid rx time, all the channels have the same RX timestamp (common RX time pseudoranges)
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std::cout<<"Ch PVT = "<< i << ", d_TOW = " << d_TOW_at_curr_symbol_constellation<<", rx_time_hybrid_PVT = " << d_rx_time << " same RX timestamp (common RX time pseudoranges)"<< std::endl;
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std::cout<<"CH PVT = "<< i << ", d_TOW = " << d_TOW_at_curr_symbol_constellation<<", rx_time_hybrid_PVT = " << d_rx_time << " same RX timestamp (common RX time pseudoranges)"<< std::endl;
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}
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}
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@ -205,7 +205,7 @@ int hybrid_pvt_cc::general_work (int noutput_items, gr_vector_int &ninput_items,
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{
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bool pvt_result;
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pvt_result = d_ls_pvt->get_PVT(gnss_pseudoranges_map, d_rx_time, d_flag_averaging);
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std::cout << "pvt_result = " << pvt_result << std::endl;
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if (pvt_result == true)
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{
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@ -40,7 +40,8 @@ hybrid_ls_pvt::hybrid_ls_pvt(int nchannels, std::string dump_filename, bool flag
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{
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// init empty ephemeris for all the available GNSS channels
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d_nchannels = nchannels;
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d_ephemeris = new Galileo_Navigation_Message[nchannels];
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d_Gal_ephemeris = new Galileo_Navigation_Message[nchannels];
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d_GPS_ephemeris = new Gps_Navigation_Message[nchannels];
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d_dump_filename = dump_filename;
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d_flag_dump_enabled = flag_dump_to_file;
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d_averaging_depth = 0;
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@ -75,7 +76,8 @@ void hybrid_ls_pvt::set_averaging_depth(int depth)
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hybrid_ls_pvt::~hybrid_ls_pvt()
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{
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d_dump_file.close();
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delete[] d_ephemeris;
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delete[] d_Gal_ephemeris;
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delete[] d_GPS_ephemeris;
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}
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@ -215,10 +217,11 @@ arma::vec hybrid_ls_pvt::leastSquarePos(arma::mat satpos, arma::vec obs, arma::m
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}
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bool hybrid_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map, double galileo_current_time, bool flag_averaging)
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bool hybrid_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map, double hybrid_current_time, bool flag_averaging)
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{
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std::map<int,Gnss_Synchro>::iterator gnss_pseudoranges_iter;
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std::map<int,Galileo_Ephemeris>::iterator galileo_ephemeris_iter;
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std::map<int,Gps_Ephemeris>::iterator gps_ephemeris_iter;
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int valid_pseudoranges = gnss_pseudoranges_map.size();
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arma::mat W = arma::eye(valid_pseudoranges, valid_pseudoranges); //channels weights matrix
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@ -226,7 +229,9 @@ bool hybrid_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map, do
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arma::mat satpos = arma::zeros(3, valid_pseudoranges); //satellite positions matrix
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int Galileo_week_number = 0;
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int GPS_week;
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double utc = 0;
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double utc_tx_corrected = 0; //utc computed at tx_time_corrected, added for Galileo constellation (in GPS utc is directly computed at TX_time_corrected_s)
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double SV_clock_drift_s = 0;
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double SV_relativistic_clock_corr_s = 0;
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double TX_time_corrected_s;
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@ -243,79 +248,165 @@ bool hybrid_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map, do
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gnss_pseudoranges_iter != gnss_pseudoranges_map.end();
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gnss_pseudoranges_iter++)
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{
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// 1- find the ephemeris for the current SV observation. The SV PRN ID is the map key
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galileo_ephemeris_iter = galileo_ephemeris_map.find(gnss_pseudoranges_iter->first);
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if (galileo_ephemeris_iter != galileo_ephemeris_map.end())
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{
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/*!
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* \todo Place here the satellite CN0 (power level, or weight factor)
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*/
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W(obs_counter, obs_counter) = 1;
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// COMMON RX TIME PVT ALGORITHM MODIFICATION (Like RINEX files)
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// first estimate of transmit time
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//Galileo_week_number = galileo_ephemeris_iter->second.WN_5;//for GST
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//double sec_in_day = 86400;
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//double day_in_week = 7;
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// t = WN*sec_in_day*day_in_week + TOW; // t is Galileo System Time to use to compute satellite positions
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if (gnss_pseudoranges_iter->second.System == 'E')
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{
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std::cout << "Satellite System: " << gnss_pseudoranges_iter->second.System <<std::endl;
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// 1 Gal - find the ephemeris for the current GALILEO SV observation. The SV PRN ID is the map key
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galileo_ephemeris_iter = galileo_ephemeris_map.find(gnss_pseudoranges_iter->first);
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if (galileo_ephemeris_iter != galileo_ephemeris_map.end())
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{
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/*!
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* \todo Place here the satellite CN0 (power level, or weight factor)
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*/
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W(obs_counter, obs_counter) = 1;
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//JAVIER VERSION:
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double Rx_time = galileo_current_time;
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// COMMON RX TIME PVT ALGORITHM MODIFICATION (Like RINEX files)
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// first estimate of transmit time
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//Galileo_week_number = galileo_ephemeris_iter->second.WN_5;//for GST
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//double sec_in_day = 86400;
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//double day_in_week = 7;
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// t = WN*sec_in_day*day_in_week + TOW; // t is Galileo System Time to use to compute satellite positions
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//to compute satellite position we need GST = WN+TOW (everything expressed in seconds)
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//double Rx_time = galileo_current_time + Galileo_week_number*sec_in_day*day_in_week;
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//JAVIER VERSION:
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double Rx_time = hybrid_current_time;
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std::cout<<"Gal_Rx_time = "<< Rx_time << std::endl;
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//to compute satellite position we need GST = WN+TOW (everything expressed in seconds)
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//double Rx_time = galileo_current_time + Galileo_week_number*sec_in_day*day_in_week;
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double Tx_time = Rx_time - gnss_pseudoranges_iter->second.Pseudorange_m/GALILEO_C_m_s;
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double Tx_time = Rx_time - gnss_pseudoranges_iter->second.Pseudorange_m/GALILEO_C_m_s;
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//std::cout<<"Gal_Tx_time = "<< Tx_time << std::endl;
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// 2- compute the clock drift using the clock model (broadcast) for this SV
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SV_clock_drift_s = galileo_ephemeris_iter->second.sv_clock_drift(Tx_time);
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// 2- compute the clock drift using the clock model (broadcast) for this SV
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SV_clock_drift_s = galileo_ephemeris_iter->second.sv_clock_drift(Tx_time);
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// 3- compute the relativistic clock drift using the clock model (broadcast) for this SV
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SV_relativistic_clock_corr_s = galileo_ephemeris_iter->second.sv_clock_relativistic_term(Tx_time);
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// 3- compute the relativistic clock drift using the clock model (broadcast) for this SV
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SV_relativistic_clock_corr_s = galileo_ephemeris_iter->second.sv_clock_relativistic_term(Tx_time);
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// 4- compute the current ECEF position for this SV using corrected TX time
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SV_clock_bias_s = SV_clock_drift_s + SV_relativistic_clock_corr_s;
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// 4- compute the current ECEF position for this SV using corrected TX time
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SV_clock_bias_s = SV_clock_drift_s + SV_relativistic_clock_corr_s;
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TX_time_corrected_s = Tx_time - SV_clock_bias_s;
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galileo_ephemeris_iter->second.satellitePosition(TX_time_corrected_s);
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TX_time_corrected_s = Tx_time - SV_clock_bias_s;
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//std::cout<<"Gal_TX_time_corrected_s = "<< TX_time_corrected_s << std::endl;
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galileo_ephemeris_iter->second.satellitePosition(TX_time_corrected_s);
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satpos(0,obs_counter) = galileo_ephemeris_iter->second.d_satpos_X;
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satpos(1,obs_counter) = galileo_ephemeris_iter->second.d_satpos_Y;
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satpos(2,obs_counter) = galileo_ephemeris_iter->second.d_satpos_Z;
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satpos(0,obs_counter) = galileo_ephemeris_iter->second.d_satpos_X;
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satpos(1,obs_counter) = galileo_ephemeris_iter->second.d_satpos_Y;
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satpos(2,obs_counter) = galileo_ephemeris_iter->second.d_satpos_Z;
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// 5- fill the observations vector with the corrected pseudoranges
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obs(obs_counter) = gnss_pseudoranges_iter->second.Pseudorange_m + SV_clock_bias_s*GALILEO_C_m_s;
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d_visible_satellites_IDs[valid_obs] = galileo_ephemeris_iter->second.i_satellite_PRN;
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d_visible_satellites_CN0_dB[valid_obs] = gnss_pseudoranges_iter->second.CN0_dB_hz;
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valid_obs++;
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// 5- fill the observations vector with the corrected pseudoranges
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obs(obs_counter) = gnss_pseudoranges_iter->second.Pseudorange_m + SV_clock_bias_s*GALILEO_C_m_s;
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d_visible_satellites_IDs[valid_obs] = galileo_ephemeris_iter->second.i_satellite_PRN;
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d_visible_satellites_CN0_dB[valid_obs] = gnss_pseudoranges_iter->second.CN0_dB_hz;
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valid_obs++;
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Galileo_week_number = galileo_ephemeris_iter->second.WN_5; //for GST
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Galileo_week_number = galileo_ephemeris_iter->second.WN_5; //for GST
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//debug
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double GST = galileo_ephemeris_iter->second.Galileo_System_Time(Galileo_week_number, galileo_current_time);
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utc = galileo_utc_model.GST_to_UTC_time(GST, Galileo_week_number);
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// get time string gregorian calendar
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boost::posix_time::time_duration t = boost::posix_time::seconds(utc);
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// 22 August 1999 00:00 last Galileo start GST epoch (ICD sec 5.1.2)
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boost::posix_time::ptime p_time(boost::gregorian::date(1999, 8, 22), t);
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d_position_UTC_time = p_time;
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LOG(INFO) << "Galileo RX time at " << boost::posix_time::to_simple_string(p_time);
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//end debug
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//debug
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double GST = galileo_ephemeris_iter->second.Galileo_System_Time(Galileo_week_number, hybrid_current_time);
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utc = galileo_utc_model.GST_to_UTC_time(GST, Galileo_week_number); // this shoud be removed and it should be considered the utc_tx_corrected
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utc_tx_corrected = galileo_utc_model.GST_to_UTC_time(TX_time_corrected_s, Galileo_week_number);
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//std::cout<<"Gal UTC at TX_time_corrected_s = "<<utc_tx_corrected<< std::endl;
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//std::cout<<"Gal_week = "<<Galileo_week_number<< std::endl;
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//std::cout << "Gal UTC = " << utc << std::endl;
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// get time string gregorian calendar
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boost::posix_time::time_duration t = boost::posix_time::seconds(utc);
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// 22 August 1999 00:00 last Galileo start GST epoch (ICD sec 5.1.2)
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boost::posix_time::ptime p_time(boost::gregorian::date(1999, 8, 22), t);
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d_position_UTC_time = p_time;
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LOG(INFO) << "Galileo RX time at " << boost::posix_time::to_simple_string(p_time);
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//end debug
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// SV ECEF DEBUG OUTPUT
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LOG(INFO) << "ECEF satellite SV ID=" << galileo_ephemeris_iter->second.i_satellite_PRN
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<< " X=" << galileo_ephemeris_iter->second.d_satpos_X
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<< " [m] Y=" << galileo_ephemeris_iter->second.d_satpos_Y
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<< " [m] Z=" << galileo_ephemeris_iter->second.d_satpos_Z
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<< " [m] PR_obs=" << obs(obs_counter) << " [m]";
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std::cout<<"E"<<galileo_ephemeris_iter->second.i_satellite_PRN<< " satellite position computed"<< std::endl;
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}
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else // the ephemeris are not available for this SV
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{
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// no valid pseudorange for the current SV
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W(obs_counter, obs_counter) = 0; // SV de-activated
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obs(obs_counter) = 1; // to avoid algorithm problems (divide by zero)
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DLOG(INFO) << "No ephemeris data for SV " << gnss_pseudoranges_iter->first;
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}
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}
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else if (gnss_pseudoranges_iter->second.System == 'G')
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{
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std::cout << "Satellite System: " << gnss_pseudoranges_iter->second.System <<std::endl;
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// 1 GPS - find the ephemeris for the current GPS SV observation. The SV PRN ID is the map key
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gps_ephemeris_iter = gps_ephemeris_map.find(gnss_pseudoranges_iter->first);
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if (gps_ephemeris_iter != gps_ephemeris_map.end())
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{
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/*!
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* \todo Place here the satellite CN0 (power level, or weight factor)
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*/
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W(obs_counter, obs_counter) = 1;
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// COMMON RX TIME PVT ALGORITHM MODIFICATION (Like RINEX files)
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// first estimate of transmit time
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double Rx_time = hybrid_current_time;
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std::cout<<"Gps_Rx_time = "<< Rx_time << std::endl;
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double Tx_time = Rx_time - gnss_pseudoranges_iter->second.Pseudorange_m/GPS_C_m_s;
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//std::cout<<"Gps_Tx_time = "<< Tx_time << std::endl;
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// 2- compute the clock drift using the clock model (broadcast) for this SV
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SV_clock_drift_s = gps_ephemeris_iter->second.sv_clock_drift(Tx_time);
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// 3- compute the relativistic clock drift using the clock model (broadcast) for this SV
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SV_relativistic_clock_corr_s = gps_ephemeris_iter->second.sv_clock_relativistic_term(Tx_time);
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// 4- compute the current ECEF position for this SV using corrected TX time
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SV_clock_bias_s = SV_clock_drift_s + SV_relativistic_clock_corr_s - gps_ephemeris_iter->second.d_TGD;
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TX_time_corrected_s = Tx_time - SV_clock_bias_s;
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gps_ephemeris_iter->second.satellitePosition(TX_time_corrected_s);
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satpos(0, obs_counter) = gps_ephemeris_iter->second.d_satpos_X;
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satpos(1, obs_counter) = gps_ephemeris_iter->second.d_satpos_Y;
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satpos(2, obs_counter) = gps_ephemeris_iter->second.d_satpos_Z;
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// 5- fill the observations vector with the corrected pseudorranges
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obs(obs_counter) = gnss_pseudoranges_iter->second.Pseudorange_m + SV_clock_bias_s*GPS_C_m_s;
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d_visible_satellites_IDs[valid_obs] = gps_ephemeris_iter->second.i_satellite_PRN;
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d_visible_satellites_CN0_dB[valid_obs] = gnss_pseudoranges_iter->second.CN0_dB_hz;
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valid_obs++;
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// SV ECEF DEBUG OUTPUT
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LOG(INFO) << "(new)ECEF satellite SV ID=" << gps_ephemeris_iter->second.i_satellite_PRN
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<< " X=" << gps_ephemeris_iter->second.d_satpos_X
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<< " [m] Y=" << gps_ephemeris_iter->second.d_satpos_Y
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<< " [m] Z=" << gps_ephemeris_iter->second.d_satpos_Z
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<< " [m] PR_obs=" << obs(obs_counter) << " [m]";
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std::cout<<"G"<<gps_ephemeris_iter->second.i_satellite_PRN<< " satellite position computed"<< std::endl;
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// compute the UTC time for this SV (just to print the asociated UTC timestamp)
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GPS_week = gps_ephemeris_iter->second.i_GPS_week;
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//std::cout<<"GPS_week = "<< GPS_week << std::endl;
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utc = gps_utc_model.utc_time(TX_time_corrected_s, GPS_week);
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//std::cout << "GPS UTC at TX_time_corrected_s= " << utc << std::endl;
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}
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else // the ephemeris are not available for this SV
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{
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// no valid pseudorange for the current SV
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W(obs_counter, obs_counter) = 0; // SV de-activated
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obs(obs_counter) = 1; // to avoid algorithm problems (divide by zero)
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DLOG(INFO) << "No ephemeris data for SV " << gnss_pseudoranges_iter->first;
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}
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}
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obs_counter++;
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std::cout<<"Number of observations in PVT = " << obs_counter << std::endl;
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// SV ECEF DEBUG OUTPUT
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LOG(INFO) << "ECEF satellite SV ID=" << galileo_ephemeris_iter->second.i_satellite_PRN
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<< " X=" << galileo_ephemeris_iter->second.d_satpos_X
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<< " [m] Y=" << galileo_ephemeris_iter->second.d_satpos_Y
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<< " [m] Z=" << galileo_ephemeris_iter->second.d_satpos_Z
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<< " [m] PR_obs=" << obs(obs_counter) << " [m]";
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}
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else // the ephemeris are not available for this SV
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{
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// no valid pseudorange for the current SV
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W(obs_counter, obs_counter) = 0; // SV de-activated
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obs(obs_counter) = 1; // to avoid algorithm problems (divide by zero)
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DLOG(INFO) << "No ephemeris data for SV "<< gnss_pseudoranges_iter->first;
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}
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obs_counter++;
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}
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// ********************************************************************************
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// ****** SOLVE LEAST SQUARES******************************************************
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@ -325,163 +416,164 @@ bool hybrid_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map, do
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if (valid_obs >= 4)
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{
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arma::vec mypos;
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DLOG(INFO) << "satpos=" << satpos;
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DLOG(INFO) << "obs="<< obs;
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DLOG(INFO) << "W=" << W;
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mypos = leastSquarePos(satpos, obs, W);
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// Compute GST and Gregorian time
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double GST = galileo_ephemeris_iter->second.Galileo_System_Time(Galileo_week_number, galileo_current_time);
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utc = galileo_utc_model.GST_to_UTC_time(GST, Galileo_week_number);
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// get time string Gregorian calendar
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boost::posix_time::time_duration t = boost::posix_time::seconds(utc);
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// 22 August 1999 00:00 last Galileo start GST epoch (ICD sec 5.1.2)
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boost::posix_time::ptime p_time(boost::gregorian::date(1999, 8, 22), t);
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d_position_UTC_time = p_time;
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LOG(INFO) << "Galileo Position at TOW=" << galileo_current_time << " in ECEF (X,Y,Z) = " << mypos;
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cart2geo((double)mypos(0), (double)mypos(1), (double)mypos(2), 4);
|
||||
//ToDo: Find an Observables/PVT random bug with some satellite configurations that gives an erratic PVT solution (i.e. height>50 km)
|
||||
if (d_height_m > 50000)
|
||||
{
|
||||
b_valid_position = false;
|
||||
return false;
|
||||
}
|
||||
LOG(INFO) << "Galileo Position at " << boost::posix_time::to_simple_string(p_time)
|
||||
<< " is Lat = " << d_latitude_d << " [deg], Long = " << d_longitude_d
|
||||
<< " [deg], Height= " << d_height_m << " [m]";
|
||||
|
||||
std::cout << "Galileo Position at " << boost::posix_time::to_simple_string(p_time)
|
||||
<< " is Lat = " << d_latitude_d << " [deg], Long = " << d_longitude_d
|
||||
<< " [deg], Height= " << d_height_m << " [m]" << std::endl;
|
||||
|
||||
// ###### Compute DOPs ########
|
||||
// 1- Rotation matrix from ECEF coordinates to ENU coordinates
|
||||
// ref: http://www.navipedia.net/index.php/Transformations_between_ECEF_and_ENU_coordinates
|
||||
arma::mat F = arma::zeros(3,3);
|
||||
F(0,0) = -sin(GPS_TWO_PI*(d_longitude_d/360.0));
|
||||
F(0,1) = -sin(GPS_TWO_PI*(d_latitude_d/360.0))*cos(GPS_TWO_PI*(d_longitude_d/360.0));
|
||||
F(0,2) = cos(GPS_TWO_PI*(d_latitude_d/360.0))*cos(GPS_TWO_PI*(d_longitude_d/360.0));
|
||||
|
||||
F(1,0) = cos((GPS_TWO_PI*d_longitude_d)/360.0);
|
||||
F(1,1) = -sin((GPS_TWO_PI*d_latitude_d)/360.0)*sin((GPS_TWO_PI*d_longitude_d)/360.0);
|
||||
F(1,2) = cos((GPS_TWO_PI*d_latitude_d/360.0))*sin((GPS_TWO_PI*d_longitude_d)/360.0);
|
||||
|
||||
F(2,0) = 0;
|
||||
F(2,1) = cos((GPS_TWO_PI*d_latitude_d)/360.0);
|
||||
F(2,2) = sin((GPS_TWO_PI*d_latitude_d/360.0));
|
||||
|
||||
// 2- Apply the rotation to the latest covariance matrix (available in ECEF from LS)
|
||||
arma::mat Q_ECEF = d_Q.submat(0, 0, 2, 2);
|
||||
arma::mat DOP_ENU = arma::zeros(3, 3);
|
||||
|
||||
try
|
||||
{
|
||||
DOP_ENU = arma::htrans(F)*Q_ECEF*F;
|
||||
d_GDOP = sqrt(arma::trace(DOP_ENU)); // Geometric DOP
|
||||
d_PDOP = sqrt(DOP_ENU(0,0) + DOP_ENU(1,1) + DOP_ENU(2,2)); // PDOP
|
||||
d_HDOP = sqrt(DOP_ENU(0,0) + DOP_ENU(1,1)); // HDOP
|
||||
d_VDOP = sqrt(DOP_ENU(2,2)); // VDOP
|
||||
d_TDOP = sqrt(d_Q(3,3)); // TDOP
|
||||
}
|
||||
catch(std::exception& ex)
|
||||
{
|
||||
d_GDOP = -1; // Geometric DOP
|
||||
d_PDOP = -1; // PDOP
|
||||
d_HDOP = -1; // HDOP
|
||||
d_VDOP = -1; // VDOP
|
||||
d_TDOP = -1; // TDOP
|
||||
}
|
||||
|
||||
// ######## LOG FILE #########
|
||||
if(d_flag_dump_enabled == true)
|
||||
{
|
||||
// MULTIPLEXED FILE RECORDING - Record results to file
|
||||
try
|
||||
{
|
||||
double tmp_double;
|
||||
// PVT GPS time
|
||||
tmp_double = galileo_current_time;
|
||||
d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// ECEF User Position East [m]
|
||||
tmp_double = mypos(0);
|
||||
d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// ECEF User Position North [m]
|
||||
tmp_double = mypos(1);
|
||||
d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// ECEF User Position Up [m]
|
||||
tmp_double = mypos(2);
|
||||
d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// User clock offset [s]
|
||||
tmp_double = mypos(3);
|
||||
d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// GEO user position Latitude [deg]
|
||||
tmp_double = d_latitude_d;
|
||||
d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// GEO user position Longitude [deg]
|
||||
tmp_double = d_longitude_d;
|
||||
d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// GEO user position Height [m]
|
||||
tmp_double = d_height_m;
|
||||
d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
}
|
||||
catch (const std::ifstream::failure& e)
|
||||
{
|
||||
LOG(WARNING) << "Exception writing PVT LS dump file "<< e.what();
|
||||
}
|
||||
}
|
||||
|
||||
// MOVING AVERAGE PVT
|
||||
if (flag_averaging == true)
|
||||
{
|
||||
if (d_hist_longitude_d.size() == (unsigned int)d_averaging_depth)
|
||||
{
|
||||
// Pop oldest value
|
||||
d_hist_longitude_d.pop_back();
|
||||
d_hist_latitude_d.pop_back();
|
||||
d_hist_height_m.pop_back();
|
||||
// Push new values
|
||||
d_hist_longitude_d.push_front(d_longitude_d);
|
||||
d_hist_latitude_d.push_front(d_latitude_d);
|
||||
d_hist_height_m.push_front(d_height_m);
|
||||
|
||||
d_avg_latitude_d = 0;
|
||||
d_avg_longitude_d = 0;
|
||||
d_avg_height_m = 0;
|
||||
for (unsigned int i = 0; i < d_hist_longitude_d.size(); i++)
|
||||
{
|
||||
d_avg_latitude_d = d_avg_latitude_d + d_hist_latitude_d.at(i);
|
||||
d_avg_longitude_d = d_avg_longitude_d + d_hist_longitude_d.at(i);
|
||||
d_avg_height_m = d_avg_height_m + d_hist_height_m.at(i);
|
||||
}
|
||||
d_avg_latitude_d = d_avg_latitude_d / (double)d_averaging_depth;
|
||||
d_avg_longitude_d = d_avg_longitude_d / (double)d_averaging_depth;
|
||||
d_avg_height_m = d_avg_height_m / (double)d_averaging_depth;
|
||||
b_valid_position = true;
|
||||
return true; //indicates that the returned position is valid
|
||||
}
|
||||
else
|
||||
{
|
||||
// int current_depth=d_hist_longitude_d.size();
|
||||
// Push new values
|
||||
d_hist_longitude_d.push_front(d_longitude_d);
|
||||
d_hist_latitude_d.push_front(d_latitude_d);
|
||||
d_hist_height_m.push_front(d_height_m);
|
||||
|
||||
d_avg_latitude_d = d_latitude_d;
|
||||
d_avg_longitude_d = d_longitude_d;
|
||||
d_avg_height_m = d_height_m;
|
||||
b_valid_position = false;
|
||||
return false; //indicates that the returned position is not valid yet
|
||||
}
|
||||
}
|
||||
else
|
||||
{
|
||||
b_valid_position = true;
|
||||
return true; //indicates that the returned position is valid
|
||||
}
|
||||
}
|
||||
// arma::vec mypos;
|
||||
// DLOG(INFO) << "satpos=" << satpos;
|
||||
// DLOG(INFO) << "obs="<< obs;
|
||||
// DLOG(INFO) << "W=" << W;
|
||||
// mypos = leastSquarePos(satpos, obs, W);
|
||||
//
|
||||
// // Compute GST and Gregorian time
|
||||
// double GST = galileo_ephemeris_iter->second.Galileo_System_Time(Galileo_week_number, hybrid_current_time);
|
||||
// utc = galileo_utc_model.GST_to_UTC_time(GST, Galileo_week_number);
|
||||
// // get time string Gregorian calendar
|
||||
// boost::posix_time::time_duration t = boost::posix_time::seconds(utc);
|
||||
// // 22 August 1999 00:00 last Galileo start GST epoch (ICD sec 5.1.2)
|
||||
// boost::posix_time::ptime p_time(boost::gregorian::date(1999, 8, 22), t);
|
||||
// d_position_UTC_time = p_time;
|
||||
// LOG(INFO) << "Galileo Position at TOW=" << hybrid_current_time << " in ECEF (X,Y,Z) = " << mypos;
|
||||
//
|
||||
// cart2geo((double)mypos(0), (double)mypos(1), (double)mypos(2), 4);
|
||||
// //ToDo: Find an Observables/PVT random bug with some satellite configurations that gives an erratic PVT solution (i.e. height>50 km)
|
||||
// if (d_height_m > 50000)
|
||||
// {
|
||||
// b_valid_position = false;
|
||||
// return false;
|
||||
// }
|
||||
// LOG(INFO) << "Galileo Position at " << boost::posix_time::to_simple_string(p_time)
|
||||
// << " is Lat = " << d_latitude_d << " [deg], Long = " << d_longitude_d
|
||||
// << " [deg], Height= " << d_height_m << " [m]";
|
||||
//
|
||||
// std::cout << "Galileo Position at " << boost::posix_time::to_simple_string(p_time)
|
||||
// << " is Lat = " << d_latitude_d << " [deg], Long = " << d_longitude_d
|
||||
// << " [deg], Height= " << d_height_m << " [m]" << std::endl;
|
||||
//
|
||||
// // ###### Compute DOPs ########
|
||||
// // 1- Rotation matrix from ECEF coordinates to ENU coordinates
|
||||
// // ref: http://www.navipedia.net/index.php/Transformations_between_ECEF_and_ENU_coordinates
|
||||
// arma::mat F = arma::zeros(3,3);
|
||||
// F(0,0) = -sin(GPS_TWO_PI*(d_longitude_d/360.0));
|
||||
// F(0,1) = -sin(GPS_TWO_PI*(d_latitude_d/360.0))*cos(GPS_TWO_PI*(d_longitude_d/360.0));
|
||||
// F(0,2) = cos(GPS_TWO_PI*(d_latitude_d/360.0))*cos(GPS_TWO_PI*(d_longitude_d/360.0));
|
||||
//
|
||||
// F(1,0) = cos((GPS_TWO_PI*d_longitude_d)/360.0);
|
||||
// F(1,1) = -sin((GPS_TWO_PI*d_latitude_d)/360.0)*sin((GPS_TWO_PI*d_longitude_d)/360.0);
|
||||
// F(1,2) = cos((GPS_TWO_PI*d_latitude_d/360.0))*sin((GPS_TWO_PI*d_longitude_d)/360.0);
|
||||
//
|
||||
// F(2,0) = 0;
|
||||
// F(2,1) = cos((GPS_TWO_PI*d_latitude_d)/360.0);
|
||||
// F(2,2) = sin((GPS_TWO_PI*d_latitude_d/360.0));
|
||||
//
|
||||
// // 2- Apply the rotation to the latest covariance matrix (available in ECEF from LS)
|
||||
// arma::mat Q_ECEF = d_Q.submat(0, 0, 2, 2);
|
||||
// arma::mat DOP_ENU = arma::zeros(3, 3);
|
||||
//
|
||||
// try
|
||||
// {
|
||||
// DOP_ENU = arma::htrans(F)*Q_ECEF*F;
|
||||
// d_GDOP = sqrt(arma::trace(DOP_ENU)); // Geometric DOP
|
||||
// d_PDOP = sqrt(DOP_ENU(0,0) + DOP_ENU(1,1) + DOP_ENU(2,2)); // PDOP
|
||||
// d_HDOP = sqrt(DOP_ENU(0,0) + DOP_ENU(1,1)); // HDOP
|
||||
// d_VDOP = sqrt(DOP_ENU(2,2)); // VDOP
|
||||
// d_TDOP = sqrt(d_Q(3,3)); // TDOP
|
||||
// }
|
||||
// catch(std::exception& ex)
|
||||
// {
|
||||
// d_GDOP = -1; // Geometric DOP
|
||||
// d_PDOP = -1; // PDOP
|
||||
// d_HDOP = -1; // HDOP
|
||||
// d_VDOP = -1; // VDOP
|
||||
// d_TDOP = -1; // TDOP
|
||||
// }
|
||||
//
|
||||
// // ######## LOG FILE #########
|
||||
// if(d_flag_dump_enabled == true)
|
||||
// {
|
||||
// // MULTIPLEXED FILE RECORDING - Record results to file
|
||||
// try
|
||||
// {
|
||||
// double tmp_double;
|
||||
// // PVT GPS time
|
||||
// tmp_double = hybrid_current_time;
|
||||
// d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// // ECEF User Position East [m]
|
||||
// tmp_double = mypos(0);
|
||||
// d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// // ECEF User Position North [m]
|
||||
// tmp_double = mypos(1);
|
||||
// d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// // ECEF User Position Up [m]
|
||||
// tmp_double = mypos(2);
|
||||
// d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// // User clock offset [s]
|
||||
// tmp_double = mypos(3);
|
||||
// d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// // GEO user position Latitude [deg]
|
||||
// tmp_double = d_latitude_d;
|
||||
// d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// // GEO user position Longitude [deg]
|
||||
// tmp_double = d_longitude_d;
|
||||
// d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// // GEO user position Height [m]
|
||||
// tmp_double = d_height_m;
|
||||
// d_dump_file.write((char*)&tmp_double, sizeof(double));
|
||||
// }
|
||||
// catch (const std::ifstream::failure& e)
|
||||
// {
|
||||
// LOG(WARNING) << "Exception writing PVT LS dump file "<< e.what();
|
||||
// }
|
||||
// }
|
||||
//
|
||||
// // MOVING AVERAGE PVT
|
||||
// if (flag_averaging == true)
|
||||
// {
|
||||
// if (d_hist_longitude_d.size() == (unsigned int)d_averaging_depth)
|
||||
// {
|
||||
// // Pop oldest value
|
||||
// d_hist_longitude_d.pop_back();
|
||||
// d_hist_latitude_d.pop_back();
|
||||
// d_hist_height_m.pop_back();
|
||||
// // Push new values
|
||||
// d_hist_longitude_d.push_front(d_longitude_d);
|
||||
// d_hist_latitude_d.push_front(d_latitude_d);
|
||||
// d_hist_height_m.push_front(d_height_m);
|
||||
//
|
||||
// d_avg_latitude_d = 0;
|
||||
// d_avg_longitude_d = 0;
|
||||
// d_avg_height_m = 0;
|
||||
// for (unsigned int i = 0; i < d_hist_longitude_d.size(); i++)
|
||||
// {
|
||||
// d_avg_latitude_d = d_avg_latitude_d + d_hist_latitude_d.at(i);
|
||||
// d_avg_longitude_d = d_avg_longitude_d + d_hist_longitude_d.at(i);
|
||||
// d_avg_height_m = d_avg_height_m + d_hist_height_m.at(i);
|
||||
// }
|
||||
// d_avg_latitude_d = d_avg_latitude_d / (double)d_averaging_depth;
|
||||
// d_avg_longitude_d = d_avg_longitude_d / (double)d_averaging_depth;
|
||||
// d_avg_height_m = d_avg_height_m / (double)d_averaging_depth;
|
||||
// b_valid_position = true;
|
||||
// return true; //indicates that the returned position is valid
|
||||
// }
|
||||
// else
|
||||
// {
|
||||
// // int current_depth=d_hist_longitude_d.size();
|
||||
// // Push new values
|
||||
// d_hist_longitude_d.push_front(d_longitude_d);
|
||||
// d_hist_latitude_d.push_front(d_latitude_d);
|
||||
// d_hist_height_m.push_front(d_height_m);
|
||||
//
|
||||
// d_avg_latitude_d = d_latitude_d;
|
||||
// d_avg_longitude_d = d_longitude_d;
|
||||
// d_avg_height_m = d_height_m;
|
||||
// b_valid_position = false;
|
||||
// return false; //indicates that the returned position is not valid yet
|
||||
// }
|
||||
// }
|
||||
// else
|
||||
// {
|
||||
// b_valid_position = true;
|
||||
// return true; //indicates that the returned position is valid
|
||||
// }
|
||||
}
|
||||
else
|
||||
{
|
||||
b_valid_position = false;
|
||||
|
|
|
|||
|
|
@ -74,8 +74,8 @@ public:
|
|||
double d_visible_satellites_Distance[PVT_MAX_CHANNELS]; //!< Array with the LOS Distance of the valid satellites
|
||||
double d_visible_satellites_CN0_dB[PVT_MAX_CHANNELS]; //!< Array with the IDs of the valid satellites
|
||||
|
||||
Galileo_Navigation_Message* d_ephemeris;
|
||||
//Gps_Navigation_Message* d_ephemeris;
|
||||
Galileo_Navigation_Message* d_Gal_ephemeris;
|
||||
Gps_Navigation_Message* d_GPS_ephemeris;
|
||||
|
||||
std::map<int,Galileo_Ephemeris> galileo_ephemeris_map; //!< Map storing new Galileo_Ephemeris
|
||||
std::map<int,Gps_Ephemeris> gps_ephemeris_map; //!< Map storing new Galileo_Ephemeris
|
||||
|
|
@ -127,7 +127,7 @@ public:
|
|||
|
||||
~hybrid_ls_pvt();
|
||||
|
||||
bool get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map, double galileo_current_time, bool flag_averaging);
|
||||
bool get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map, double hybrid_current_time, bool flag_averaging);
|
||||
|
||||
/*!
|
||||
* \brief Conversion of Cartesian coordinates (X,Y,Z) to geographical
|
||||
|
|
|
|||
Loading…
Reference in New Issue