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https://github.com/gnss-sdr/gnss-sdr
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less verbose logging in Release
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@ -308,7 +308,7 @@ bool galileo_e1_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map
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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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DLOG(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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@ -345,7 +345,7 @@ bool galileo_e1_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map
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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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DLOG(INFO) << "Galileo Position at TOW=" << galileo_current_time << " in ECEF (X,Y,Z) = " << mypos;
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cart2geo(static_cast<double>(mypos(0)), static_cast<double>(mypos(1)), static_cast<double>(mypos(2)), 4);
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//ToDo: Find an Observables/PVT random bug with some satellite configurations that gives an erratic PVT solution (i.e. height>50 km)
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@ -289,7 +289,7 @@ bool gps_l1_ca_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map,
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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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DLOG(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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@ -318,11 +318,11 @@ bool gps_l1_ca_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map,
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if (valid_obs >= 4)
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{
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arma::vec mypos;
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LOG(INFO) << "satpos=" << satpos;
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LOG(INFO) << "obs=" << obs;
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LOG(INFO) << "W=" << W;
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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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LOG(INFO) << "(new)Position at TOW=" << GPS_current_time << " in ECEF (X,Y,Z) = " << mypos;
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DLOG(INFO) << "(new)Position at TOW=" << GPS_current_time << " in ECEF (X,Y,Z) = " << mypos;
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gps_l1_ca_ls_pvt::cart2geo(mypos(0), mypos(1), mypos(2), 4);
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//ToDo: Find an Observables/PVT random bug with some satellite configurations that gives an erratic PVT solution (i.e. height>50 km)
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if (d_height_m > 50000)
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@ -318,7 +318,7 @@ bool hybrid_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map, do
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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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DLOG(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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@ -369,7 +369,7 @@ bool hybrid_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map, do
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valid_obs++;
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valid_obs_GPS_counter++;
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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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DLOG(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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@ -414,7 +414,7 @@ bool hybrid_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map, do
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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) << "HYBRID Position at TOW=" << hybrid_current_time << " in ECEF (X,Y,Z) = " << mypos;
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DLOG(INFO) << "HYBRID Position at TOW=" << hybrid_current_time << " in ECEF (X,Y,Z) = " << mypos;
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cart2geo(static_cast<double>(mypos(0)), static_cast<double>(mypos(1)), static_cast<double>(mypos(2)), 4);
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//ToDo: Find an Observables/PVT random bug with some satellite configurations that gives an erratic PVT solution (i.e. height>50 km)
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@ -178,7 +178,7 @@ void Gps_L1_Ca_Dll_Pll_Tracking_cc::start_tracking()
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long int acq_trk_diff_samples;
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float acq_trk_diff_seconds;
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acq_trk_diff_samples = static_cast<long int>(d_sample_counter) - static_cast<long int>(d_acq_sample_stamp);//-d_vector_length;
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LOG(INFO) << "Number of samples between Acquisition and Tracking =" << acq_trk_diff_samples;
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DLOG(INFO) << "Number of samples between Acquisition and Tracking =" << acq_trk_diff_samples;
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acq_trk_diff_seconds = static_cast<float>(acq_trk_diff_samples) / static_cast<float>(d_fs_in);
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//doppler effect
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// Fd=(C/(C+Vr))*F
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@ -513,9 +513,8 @@ int Gps_L1_Ca_Dll_Pll_Tracking_cc::general_work (int noutput_items, gr_vector_in
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if (floor(d_sample_counter / d_fs_in) != d_last_seg)
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{
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d_last_seg = floor(d_sample_counter / d_fs_in);
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LOG(INFO) << "Tracking CH " << d_channel << ": Satellite " << Gnss_Satellite(systemName[sys], d_acquisition_gnss_synchro->PRN)
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<< ", CN0 = " << d_CN0_SNV_dB_Hz << " [dB-Hz]";
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//std::cout<<"TRK CH "<<d_channel<<" Carrier_lock_test="<<d_carrier_lock_test<< std::endl;
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DLOG(INFO) << "Tracking CH " << d_channel << ": Satellite " << Gnss_Satellite(systemName[sys], d_acquisition_gnss_synchro->PRN)
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<< ", CN0 = " << d_CN0_SNV_dB_Hz << " [dB-Hz]";
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}
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}
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}
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@ -383,7 +383,7 @@ void GNSSFlowgraph::wait()
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*/
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void GNSSFlowgraph::apply_action(unsigned int who, unsigned int what)
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{
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LOG(INFO) << "received " << what << " from " << who;
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DLOG(INFO) << "received " << what << " from " << who;
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switch (what)
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{
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@ -418,13 +418,10 @@ void GNSSFlowgraph::apply_action(unsigned int who, unsigned int what)
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channels_.at(i)->start_acquisition();
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break;
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}
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DLOG(INFO) << "Channel " << i << " in state " << channels_state_[i];
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}
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}
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for (unsigned int i = 0; i < channels_count_; i++)
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{
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LOG(INFO) << "Channel " << i << " in state " << channels_state_[i] << std::endl;
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}
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break;
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case 2:
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@ -441,16 +438,16 @@ void GNSSFlowgraph::apply_action(unsigned int who, unsigned int what)
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channels_.at(who)->standby();
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}
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for (unsigned int i = 0; i < channels_count_; i++)
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{
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LOG(INFO) << "Channel " << i << " in state " << channels_state_[i] << std::endl;
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}
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// for (unsigned int i = 0; i < channels_count_; i++)
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// {
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// LOG(INFO) << "Channel " << i << " in state " << channels_state_[i] << std::endl;
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// }
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break;
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default:
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break;
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}
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LOG(INFO) << "Number of available satellites: " << available_GNSS_signals_.size();
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DLOG(INFO) << "Number of available satellites: " << available_GNSS_signals_.size();
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}
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@ -694,11 +691,8 @@ void GNSSFlowgraph::set_channels_state()
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}
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else
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channels_state_.push_back(0);
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DLOG(INFO) << "Channel " << i << " in state " << channels_state_[i];
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}
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acq_channels_count_ = max_acq_channels_;
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DLOG(INFO) << acq_channels_count_ << " channels in acquisition state";
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for (unsigned int i = 0; i < channels_count_; i++)
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{
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LOG(INFO) << "Channel " << i << " in state " << channels_state_[i];
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}
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}
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