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mirror of https://github.com/gnss-sdr/gnss-sdr synced 2025-01-12 18:30:34 +00:00

less verbose logging in Release

This commit is contained in:
Carles Fernandez 2015-05-04 22:16:26 +02:00
parent c9300c45a0
commit e354b1ce53
5 changed files with 21 additions and 28 deletions

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@ -308,7 +308,7 @@ bool galileo_e1_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map
//end debug //end debug
// SV ECEF DEBUG OUTPUT // SV ECEF DEBUG OUTPUT
LOG(INFO) << "ECEF satellite SV ID=" << galileo_ephemeris_iter->second.i_satellite_PRN DLOG(INFO) << "ECEF satellite SV ID=" << galileo_ephemeris_iter->second.i_satellite_PRN
<< " X=" << galileo_ephemeris_iter->second.d_satpos_X << " X=" << galileo_ephemeris_iter->second.d_satpos_X
<< " [m] Y=" << galileo_ephemeris_iter->second.d_satpos_Y << " [m] Y=" << galileo_ephemeris_iter->second.d_satpos_Y
<< " [m] Z=" << galileo_ephemeris_iter->second.d_satpos_Z << " [m] Z=" << galileo_ephemeris_iter->second.d_satpos_Z
@ -345,7 +345,7 @@ bool galileo_e1_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map
// 22 August 1999 00:00 last Galileo start GST epoch (ICD sec 5.1.2) // 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); boost::posix_time::ptime p_time(boost::gregorian::date(1999, 8, 22), t);
d_position_UTC_time = p_time; d_position_UTC_time = p_time;
LOG(INFO) << "Galileo Position at TOW=" << galileo_current_time << " in ECEF (X,Y,Z) = " << mypos; DLOG(INFO) << "Galileo Position at TOW=" << galileo_current_time << " in ECEF (X,Y,Z) = " << mypos;
cart2geo(static_cast<double>(mypos(0)), static_cast<double>(mypos(1)), static_cast<double>(mypos(2)), 4); cart2geo(static_cast<double>(mypos(0)), static_cast<double>(mypos(1)), static_cast<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) //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,
valid_obs++; valid_obs++;
// SV ECEF DEBUG OUTPUT // SV ECEF DEBUG OUTPUT
LOG(INFO) << "(new)ECEF satellite SV ID=" << gps_ephemeris_iter->second.i_satellite_PRN DLOG(INFO) << "(new)ECEF satellite SV ID=" << gps_ephemeris_iter->second.i_satellite_PRN
<< " X=" << gps_ephemeris_iter->second.d_satpos_X << " X=" << gps_ephemeris_iter->second.d_satpos_X
<< " [m] Y=" << gps_ephemeris_iter->second.d_satpos_Y << " [m] Y=" << gps_ephemeris_iter->second.d_satpos_Y
<< " [m] Z=" << gps_ephemeris_iter->second.d_satpos_Z << " [m] Z=" << gps_ephemeris_iter->second.d_satpos_Z
@ -318,11 +318,11 @@ bool gps_l1_ca_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map,
if (valid_obs >= 4) if (valid_obs >= 4)
{ {
arma::vec mypos; arma::vec mypos;
LOG(INFO) << "satpos=" << satpos; DLOG(INFO) << "satpos=" << satpos;
LOG(INFO) << "obs=" << obs; DLOG(INFO) << "obs=" << obs;
LOG(INFO) << "W=" << W; DLOG(INFO) << "W=" << W;
mypos = leastSquarePos(satpos, obs, W); mypos = leastSquarePos(satpos, obs, W);
LOG(INFO) << "(new)Position at TOW=" << GPS_current_time << " in ECEF (X,Y,Z) = " << mypos; DLOG(INFO) << "(new)Position at TOW=" << GPS_current_time << " in ECEF (X,Y,Z) = " << mypos;
gps_l1_ca_ls_pvt::cart2geo(mypos(0), mypos(1), mypos(2), 4); gps_l1_ca_ls_pvt::cart2geo(mypos(0), mypos(1), 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) //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) 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
//end debug //end debug
// SV ECEF DEBUG OUTPUT // SV ECEF DEBUG OUTPUT
LOG(INFO) << "ECEF satellite SV ID=" << galileo_ephemeris_iter->second.i_satellite_PRN DLOG(INFO) << "ECEF satellite SV ID=" << galileo_ephemeris_iter->second.i_satellite_PRN
<< " X=" << galileo_ephemeris_iter->second.d_satpos_X << " X=" << galileo_ephemeris_iter->second.d_satpos_X
<< " [m] Y=" << galileo_ephemeris_iter->second.d_satpos_Y << " [m] Y=" << galileo_ephemeris_iter->second.d_satpos_Y
<< " [m] Z=" << galileo_ephemeris_iter->second.d_satpos_Z << " [m] Z=" << galileo_ephemeris_iter->second.d_satpos_Z
@ -369,7 +369,7 @@ bool hybrid_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map, do
valid_obs++; valid_obs++;
valid_obs_GPS_counter++; valid_obs_GPS_counter++;
// SV ECEF DEBUG OUTPUT // SV ECEF DEBUG OUTPUT
LOG(INFO) << "(new)ECEF satellite SV ID=" << gps_ephemeris_iter->second.i_satellite_PRN DLOG(INFO) << "(new)ECEF satellite SV ID=" << gps_ephemeris_iter->second.i_satellite_PRN
<< " X=" << gps_ephemeris_iter->second.d_satpos_X << " X=" << gps_ephemeris_iter->second.d_satpos_X
<< " [m] Y=" << gps_ephemeris_iter->second.d_satpos_Y << " [m] Y=" << gps_ephemeris_iter->second.d_satpos_Y
<< " [m] Z=" << gps_ephemeris_iter->second.d_satpos_Z << " [m] Z=" << gps_ephemeris_iter->second.d_satpos_Z
@ -414,7 +414,7 @@ bool hybrid_ls_pvt::get_PVT(std::map<int,Gnss_Synchro> gnss_pseudoranges_map, do
// 22 August 1999 00:00 last Galileo start GST epoch (ICD sec 5.1.2) // 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); boost::posix_time::ptime p_time(boost::gregorian::date(1999, 8, 22), t);
d_position_UTC_time = p_time; d_position_UTC_time = p_time;
LOG(INFO) << "HYBRID Position at TOW=" << hybrid_current_time << " in ECEF (X,Y,Z) = " << mypos; DLOG(INFO) << "HYBRID Position at TOW=" << hybrid_current_time << " in ECEF (X,Y,Z) = " << mypos;
cart2geo(static_cast<double>(mypos(0)), static_cast<double>(mypos(1)), static_cast<double>(mypos(2)), 4); cart2geo(static_cast<double>(mypos(0)), static_cast<double>(mypos(1)), static_cast<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) //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()
long int acq_trk_diff_samples; long int acq_trk_diff_samples;
float acq_trk_diff_seconds; float acq_trk_diff_seconds;
acq_trk_diff_samples = static_cast<long int>(d_sample_counter) - static_cast<long int>(d_acq_sample_stamp);//-d_vector_length; acq_trk_diff_samples = static_cast<long int>(d_sample_counter) - static_cast<long int>(d_acq_sample_stamp);//-d_vector_length;
LOG(INFO) << "Number of samples between Acquisition and Tracking =" << acq_trk_diff_samples; DLOG(INFO) << "Number of samples between Acquisition and Tracking =" << acq_trk_diff_samples;
acq_trk_diff_seconds = static_cast<float>(acq_trk_diff_samples) / static_cast<float>(d_fs_in); acq_trk_diff_seconds = static_cast<float>(acq_trk_diff_samples) / static_cast<float>(d_fs_in);
//doppler effect //doppler effect
// Fd=(C/(C+Vr))*F // Fd=(C/(C+Vr))*F
@ -513,9 +513,8 @@ int Gps_L1_Ca_Dll_Pll_Tracking_cc::general_work (int noutput_items, gr_vector_in
if (floor(d_sample_counter / d_fs_in) != d_last_seg) if (floor(d_sample_counter / d_fs_in) != d_last_seg)
{ {
d_last_seg = floor(d_sample_counter / d_fs_in); d_last_seg = floor(d_sample_counter / d_fs_in);
LOG(INFO) << "Tracking CH " << d_channel << ": Satellite " << Gnss_Satellite(systemName[sys], d_acquisition_gnss_synchro->PRN) DLOG(INFO) << "Tracking CH " << d_channel << ": Satellite " << Gnss_Satellite(systemName[sys], d_acquisition_gnss_synchro->PRN)
<< ", CN0 = " << d_CN0_SNV_dB_Hz << " [dB-Hz]"; << ", CN0 = " << d_CN0_SNV_dB_Hz << " [dB-Hz]";
//std::cout<<"TRK CH "<<d_channel<<" Carrier_lock_test="<<d_carrier_lock_test<< std::endl;
} }
} }
} }

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@ -383,7 +383,7 @@ void GNSSFlowgraph::wait()
*/ */
void GNSSFlowgraph::apply_action(unsigned int who, unsigned int what) void GNSSFlowgraph::apply_action(unsigned int who, unsigned int what)
{ {
LOG(INFO) << "received " << what << " from " << who; DLOG(INFO) << "received " << what << " from " << who;
switch (what) switch (what)
{ {
@ -418,13 +418,10 @@ void GNSSFlowgraph::apply_action(unsigned int who, unsigned int what)
channels_.at(i)->start_acquisition(); channels_.at(i)->start_acquisition();
break; break;
} }
DLOG(INFO) << "Channel " << i << " in state " << channels_state_[i];
} }
} }
for (unsigned int i = 0; i < channels_count_; i++)
{
LOG(INFO) << "Channel " << i << " in state " << channels_state_[i] << std::endl;
}
break; break;
case 2: case 2:
@ -441,16 +438,16 @@ void GNSSFlowgraph::apply_action(unsigned int who, unsigned int what)
channels_.at(who)->standby(); channels_.at(who)->standby();
} }
for (unsigned int i = 0; i < channels_count_; i++) // for (unsigned int i = 0; i < channels_count_; i++)
{ // {
LOG(INFO) << "Channel " << i << " in state " << channels_state_[i] << std::endl; // LOG(INFO) << "Channel " << i << " in state " << channels_state_[i] << std::endl;
} // }
break; break;
default: default:
break; break;
} }
LOG(INFO) << "Number of available satellites: " << available_GNSS_signals_.size(); DLOG(INFO) << "Number of available satellites: " << available_GNSS_signals_.size();
} }
@ -694,11 +691,8 @@ void GNSSFlowgraph::set_channels_state()
} }
else else
channels_state_.push_back(0); channels_state_.push_back(0);
DLOG(INFO) << "Channel " << i << " in state " << channels_state_[i];
} }
acq_channels_count_ = max_acq_channels_; acq_channels_count_ = max_acq_channels_;
DLOG(INFO) << acq_channels_count_ << " channels in acquisition state"; DLOG(INFO) << acq_channels_count_ << " channels in acquisition state";
for (unsigned int i = 0; i < channels_count_; i++)
{
LOG(INFO) << "Channel " << i << " in state " << channels_state_[i];
}
} }