mirror of
https://github.com/gnss-sdr/gnss-sdr
synced 2024-12-12 19:20:32 +00:00
Work on the telemetry decoder to support the variable-length correlator in GPS L1 CA tracking
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@ -59,16 +59,16 @@ gps_l1_ca_make_telemetry_decoder_cc(Gnss_Satellite satellite, boost::shared_ptr<
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void gps_l1_ca_telemetry_decoder_cc::forecast (int noutput_items, gr_vector_int &ninput_items_required)
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{
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if (noutput_items != 0)
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{
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for (unsigned i = 0; i < 3; i++)
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{
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ninput_items_required[i] = d_samples_per_bit * 8; //set the required sample history
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}
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}
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}
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//void gps_l1_ca_telemetry_decoder_cc::forecast (int noutput_items, gr_vector_int &ninput_items_required)
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//{
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// if (noutput_items != 0)
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// {
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// for (unsigned i = 0; i < 3; i++)
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// {
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// ninput_items_required[i] = d_samples_per_bit * 8; //set the required sample history
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// }
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// }
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//}
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@ -181,114 +181,101 @@ int gps_l1_ca_telemetry_decoder_cc::general_work (int noutput_items, gr_vector_i
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// ########### Output the tracking data to navigation and PVT ##########
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const Gnss_Synchro **in = (const Gnss_Synchro **) &input_items[0]; //Get the input samples pointer
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// TODO Optimize me!
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if (in[0][d_samples_per_bit*8 - 1].symbol_integration_enabled==false)
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// keep the last valid symbols
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if (in[0]->Flag_valid_symbol_output==true)
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{
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//******* preamble correlation ********
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for (unsigned int i = 0; i < d_samples_per_bit*8; i++)
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d_symbol_history.push_back(in[0]->Prompt_I);
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if (static_cast<int>(d_symbol_history.size())>GPS_CA_PREAMBLE_LENGTH_SYMBOLS)
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{
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if (in[0][i].Prompt_I < 0) // symbols clipping
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{
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corr_value -= d_preambles_symbols[i];
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}
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else
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{
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corr_value += d_preambles_symbols[i];
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}
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d_symbol_history.pop_front();
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}
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}else{
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//******* preamble correlation ********
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for (unsigned int i = 0; i < d_samples_per_bit*8; i++)
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{
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if (in[0][i].Flag_valid_symbol_output==true)
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{
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if (in[0][i].Prompt_I < 0) // symbols clipping
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if (d_symbol_history.size()==GPS_CA_PREAMBLE_LENGTH_SYMBOLS)
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{
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//******* preamble correlation ********
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int current_symbol_index=0;
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for (int i = 0; i < GPS_CA_PREAMBLE_LENGTH_SYMBOLS/in[0]->correlation_length_ms; i++)
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{
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current_symbol_index=i*in[0]->correlation_length_ms;//+static_cast<int>(floor(in[0]->correlation_length_ms/2));
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if (d_symbol_history.at(i) < 0) // symbols clipping
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{
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corr_value -= d_preambles_symbols[i]*d_samples_per_bit;
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//symbol weight expansion using the current tracking correlation length
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corr_value -= d_preambles_symbols[current_symbol_index]*in[0]->correlation_length_ms;
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}
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else
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{
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corr_value += d_preambles_symbols[i]*d_samples_per_bit;
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//symbol weight expansion using the current tracking correlation length
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corr_value += d_preambles_symbols[current_symbol_index]*in[0]->correlation_length_ms;
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}
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}
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}
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}
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}
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if (abs(corr_value)>120)
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{
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std::cout<<abs(corr_value)<<std::endl;
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}
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}
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d_flag_preamble = false;
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//******* frame sync ******************
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if (abs(corr_value) == 160)
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{
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//TODO: Rewrite with state machine
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if (d_stat == 0)
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{
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d_GPS_FSM.Event_gps_word_preamble();
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d_preamble_index = d_sample_counter;//record the preamble sample stamp
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DLOG(INFO) << "Preamble detection for SAT " << this->d_satellite;
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d_symbol_accumulator = 0; //sync the symbol to bits integrator
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d_symbol_accumulator_counter = 0;
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d_frame_bit_index = 7;
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d_stat = 1; // enter into frame pre-detection status
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}
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else if (d_stat == 1) //check 6 seconds of preamble separation
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{
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preamble_diff = d_sample_counter - d_preamble_index;
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if (abs(preamble_diff - 6000) < 1)
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{
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d_GPS_FSM.Event_gps_word_preamble();
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d_flag_preamble = true;
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d_preamble_index = d_sample_counter; //record the preamble sample stamp (t_P)
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d_preamble_time_seconds = in[0][0].Tracking_timestamp_secs;// - d_preamble_duration_seconds; //record the PRN start sample index associated to the preamble
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d_frame_bit_index = 7;
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if (!d_flag_frame_sync)
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{
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//send asynchronous message to tracking to inform of frame sync and extend correlation time
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pmt::pmt_t value = pmt::from_long(d_preamble_index-1);
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this->message_port_pub(pmt::mp("preamble_index"),value);
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if (abs(corr_value) == GPS_CA_PREAMBLE_LENGTH_SYMBOLS)
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{
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if (d_stat == 0)
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{
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d_GPS_FSM.Event_gps_word_preamble();
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d_preamble_index = d_sample_counter;//record the preamble sample stamp
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std::cout << "Preamble detection for SAT " << this->d_satellite;
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d_symbol_accumulator = 0; //sync the symbol to bits integrator
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d_symbol_accumulator_counter = 0;
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d_frame_bit_index = 7;
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d_stat = 1; // enter into frame pre-detection status
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}
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else if (d_stat == 1) //check 6 seconds of preamble separation
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{
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preamble_diff = d_sample_counter - d_preamble_index;
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if (abs(preamble_diff - 6000) < 1)
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{
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std::cout <<"preamble! corr lenght="<<in[0]->correlation_length_ms<<std::endl;
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d_GPS_FSM.Event_gps_word_preamble();
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d_flag_preamble = true;
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d_preamble_index = d_sample_counter; //record the preamble sample stamp (t_P)
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d_preamble_time_seconds = in[0][0].Tracking_timestamp_secs;// - d_preamble_duration_seconds; //record the PRN start sample index associated to the preamble
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d_frame_bit_index = 7;
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if (!d_flag_frame_sync)
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{
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//send asynchronous message to tracking to inform of frame sync and extend correlation time
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pmt::pmt_t value = pmt::from_long(d_preamble_index-2);
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this->message_port_pub(pmt::mp("preamble_index"),value);
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d_flag_frame_sync = true;
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if (corr_value < 0)
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{
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flag_PLL_180_deg_phase_locked = true; //PLL is locked to opposite phase!
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DLOG(INFO) << " PLL in opposite phase for Sat "<< this->d_satellite.get_PRN();
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}
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else
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{
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flag_PLL_180_deg_phase_locked = false;
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}
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DLOG(INFO) << " Frame sync SAT " << this->d_satellite << " with preamble start at " << d_preamble_time_seconds << " [s]";
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}
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}
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}
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}
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else
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{
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if (d_stat == 1)
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{
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preamble_diff = d_sample_counter - d_preamble_index;
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if (preamble_diff > 6001)
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{
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DLOG(INFO) << "Lost of frame sync SAT " << this->d_satellite << " preamble_diff= " << preamble_diff;
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d_stat = 0; //lost of frame sync
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d_flag_frame_sync = false;
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flag_TOW_set = false;
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}
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}
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}
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d_flag_frame_sync = true;
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if (corr_value < 0)
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{
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flag_PLL_180_deg_phase_locked = true; //PLL is locked to opposite phase!
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std::cout << " PLL in opposite phase for Sat "<< this->d_satellite.get_PRN();
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}
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else
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{
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flag_PLL_180_deg_phase_locked = false;
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}
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std::cout << " Frame sync SAT " << this->d_satellite << " with preamble start at " << d_preamble_time_seconds << " [s]";
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}
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}else{
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if (preamble_diff > 6001)
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{
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std::cout << "Lost of frame sync SAT " << this->d_satellite << " preamble_diff= " << preamble_diff;
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d_stat = 0; //lost of frame sync
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d_flag_frame_sync = false;
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flag_TOW_set = false;
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}
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}
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}
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}
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//******* SYMBOL TO BIT *******
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if (in[0][d_samples_per_bit*8 - 1].Flag_valid_symbol_output==true)
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if (in[0]->Flag_valid_symbol_output==true)
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{
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if (in[0][d_samples_per_bit*8 - 1].symbol_integration_enabled==true)
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{
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// extended correlation to bit period is enabled in tracking!
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// 1 symbol = 1 bit
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d_symbol_accumulator = in[0][d_samples_per_bit*8 - 1].Prompt_I; // accumulate the input value in d_symbol_accumulator
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d_symbol_accumulator_counter=20;
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}else{
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// 20 symbols = 1 bit: do symbols integration in telemetry decoder
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d_symbol_accumulator += in[0][d_samples_per_bit*8 - 1].Prompt_I; // accumulate the input value in d_symbol_accumulator
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d_symbol_accumulator_counter++;
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}
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// extended correlation to bit period is enabled in tracking!
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d_symbol_accumulator += in[0]->Prompt_I; // accumulate the input value in d_symbol_accumulator
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d_symbol_accumulator_counter+=in[0]->correlation_length_ms;
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}
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if (d_symbol_accumulator_counter == 20 )
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@ -342,8 +329,6 @@ int gps_l1_ca_telemetry_decoder_cc::general_work (int noutput_items, gr_vector_i
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{
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d_GPS_frame_4bytes <<= 1; //shift 1 bit left the telemetry word
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}
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}
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// output the frame
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consume_each(1); //one by one
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@ -381,8 +366,8 @@ int gps_l1_ca_telemetry_decoder_cc::general_work (int noutput_items, gr_vector_i
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if (flag_PLL_180_deg_phase_locked == true)
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{
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//correct the accumulated phase for the costas loop phase shift, if required
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current_synchro_data.Carrier_phase_rads += GPS_PI;
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//correct the accumulated phase for the costas loop phase shift, if required
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current_synchro_data.Carrier_phase_rads += GPS_PI;
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}
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if(d_dump == true)
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@ -85,7 +85,7 @@ public:
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* \brief Function which tells the scheduler how many input items
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* are required to produce noutput_items output items.
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*/
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void forecast (int noutput_items, gr_vector_int &ninput_items_required);
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//void forecast (int noutput_items, gr_vector_int &ninput_items_required);
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private:
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friend gps_l1_ca_telemetry_decoder_cc_sptr
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@ -107,6 +107,7 @@ private:
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bool d_flag_frame_sync;
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// symbols
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std::deque<double> d_symbol_history;
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double d_symbol_accumulator;
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short int d_symbol_accumulator_counter;
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@ -138,10 +139,6 @@ private:
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double d_TOW_at_Preamble;
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double d_TOW_at_current_symbol;
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std::deque<double> d_symbol_TOW_queue_s;
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// Doppler and Phase accumulator queue for interpolation in Observables
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std::deque<double> d_carrier_doppler_queue_hz;
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std::deque<double> d_acc_carrier_phase_queue_rads;
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double Prn_timestamp_at_preamble_ms;
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bool flag_TOW_set;
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@ -347,6 +347,8 @@ int gps_l1_ca_dll_pll_c_aid_tracking_cc::general_work (int noutput_items, gr_vec
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d_pull_in = false;
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// Fill the acquisition data
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current_synchro_data = *d_acquisition_gnss_synchro;
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current_synchro_data.correlation_length_ms=1;
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current_synchro_data.Flag_valid_symbol_output = false;
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*out[0] = current_synchro_data;
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consume_each(samples_offset); //shift input to perform alignment with local replica
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d_symbol_counter++;
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@ -361,13 +363,13 @@ int gps_l1_ca_dll_pll_c_aid_tracking_cc::general_work (int noutput_items, gr_vec
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multicorrelator_cpu.set_input_output_vectors(d_correlator_outs,in);
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multicorrelator_cpu.Carrier_wipeoff_multicorrelator_resampler(d_rem_carrier_phase_rad, d_carrier_phase_step_rad, d_rem_code_phase_chips, d_code_phase_step_chips, d_correlation_length_samples);
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// ####### 20ms coherent intergration extension (experimental)
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// keep the last 40 symbols (2 bits to detect transitions)
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// ####### coherent intergration extension
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// keep the last symbols
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d_E_history.push_back(d_correlator_outs[0]); // save early output
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d_P_history.push_back(d_correlator_outs[1]); // save prompt output
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d_L_history.push_back(d_correlator_outs[2]); // save late output
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if (d_P_history.size()>d_extend_correlation_ms)
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if (static_cast<int>(d_P_history.size())>d_extend_correlation_ms)
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{
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d_E_history.pop_front();
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d_P_history.pop_front();
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@ -382,7 +384,6 @@ int gps_l1_ca_dll_pll_c_aid_tracking_cc::general_work (int noutput_items, gr_vec
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{
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// compute coherent integration and enable tracking loop
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// perform coherent integration using correlator output history
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//gr_complex d_correlator_outs_2[3];
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//std::cout<<"##### RESET COHERENT INTEGRATION ####"<<std::endl;
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d_correlator_outs[0]=gr_complex(0.0,0.0);
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d_correlator_outs[1]=gr_complex(0.0,0.0);
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@ -402,14 +403,11 @@ int gps_l1_ca_dll_pll_c_aid_tracking_cc::general_work (int noutput_items, gr_vec
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std::cout<<"dll="<<d_dll_bw_hz<<" dll_n="<<d_dll_bw_narrow_hz<<" pll="<<d_pll_bw_hz<<" pll_n="<<d_pll_bw_narrow_hz<<std::endl;
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}
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current_synchro_data.symbol_integration_enabled=true;
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// UPDATE INTEGRATION TIME
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CURRENT_INTEGRATION_TIME_S = static_cast<double>(d_extend_correlation_ms)*GPS_L1_CA_CODE_PERIOD;
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enable_dll_pll=true;
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}else{
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current_synchro_data.symbol_integration_enabled=false;
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if(d_preamble_synchronized==true)
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{
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// continue extended coherent correlation
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@ -434,6 +432,10 @@ int gps_l1_ca_dll_pll_c_aid_tracking_cc::general_work (int noutput_items, gr_vec
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//remnant code phase [chips]
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d_rem_code_phase_chips = d_rem_code_phase_samples * (d_code_freq_chips / static_cast<double>(d_fs_in));
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// UPDATE ACCUMULATED CARRIER PHASE
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CORRECTED_INTEGRATION_TIME_S=(static_cast<double>(d_correlation_length_samples)/static_cast<double>(d_fs_in));
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d_acc_carrier_phase_cycles -= d_carrier_doppler_hz * CORRECTED_INTEGRATION_TIME_S;
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// disable tracking loop and inform telemetry decoder
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enable_dll_pll=false;
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}else{
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@ -444,13 +446,11 @@ int gps_l1_ca_dll_pll_c_aid_tracking_cc::general_work (int noutput_items, gr_vec
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}
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}
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}else{
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current_synchro_data.symbol_integration_enabled=false;
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// UPDATE INTEGRATION TIME
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CURRENT_INTEGRATION_TIME_S = static_cast<double>(d_correlation_length_samples) / static_cast<double>(d_fs_in);
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enable_dll_pll=true;
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}
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// ###### end 20ms correlation extension
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if (enable_dll_pll==true)
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{
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@ -498,7 +498,7 @@ int gps_l1_ca_dll_pll_c_aid_tracking_cc::general_work (int noutput_items, gr_vec
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d_correlation_length_samples = K_prn_samples + d_rem_code_phase_integer_samples; //round to a discrete samples
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d_rem_code_phase_samples=d_rem_code_phase_samples-d_rem_code_phase_integer_samples;
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// UPDATE REMNANT CARRIER PHASE
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// UPDATE ACCUMULATED CARRIER PHASE
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CORRECTED_INTEGRATION_TIME_S=(static_cast<double>(d_correlation_length_samples)/static_cast<double>(d_fs_in));
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//remnant carrier phase [rad]
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d_rem_carrier_phase_rad = fmod(d_rem_carrier_phase_rad + GPS_TWO_PI * d_carrier_doppler_hz * CORRECTED_INTEGRATION_TIME_S, GPS_TWO_PI);
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@ -527,13 +527,8 @@ int gps_l1_ca_dll_pll_c_aid_tracking_cc::general_work (int noutput_items, gr_vec
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{
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d_cn0_estimation_counter = 0;
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// Code lock indicator
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if (current_synchro_data.symbol_integration_enabled==false)
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{
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d_CN0_SNV_dB_Hz = cn0_svn_estimator(d_Prompt_buffer, CN0_ESTIMATION_SAMPLES, d_fs_in, GPS_L1_CA_CODE_LENGTH_CHIPS);
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}else{
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d_CN0_SNV_dB_Hz = cn0_svn_estimator(d_Prompt_buffer, CN0_ESTIMATION_SAMPLES, d_fs_in, GPS_L1_CA_CODE_LENGTH_CHIPS*d_extend_correlation_ms);
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}
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// Carrier lock indicator
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d_CN0_SNV_dB_Hz = cn0_svn_estimator(d_Prompt_buffer, CN0_ESTIMATION_SAMPLES, d_fs_in, GPS_L1_CA_CODE_LENGTH_CHIPS);
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// Carrier lock indicator
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d_carrier_lock_test = carrier_lock_detector(d_Prompt_buffer, CN0_ESTIMATION_SAMPLES);
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// Loss of lock detection
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if (d_carrier_lock_test < d_carrier_lock_threshold or d_CN0_SNV_dB_Hz < MINIMUM_VALID_CN0)
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@ -569,6 +564,12 @@ int gps_l1_ca_dll_pll_c_aid_tracking_cc::general_work (int noutput_items, gr_vec
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current_synchro_data.CN0_dB_hz = d_CN0_SNV_dB_Hz;
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current_synchro_data.Flag_valid_pseudorange = false;
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current_synchro_data.Flag_valid_symbol_output = true;
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if (d_preamble_synchronized==true)
|
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{
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current_synchro_data.correlation_length_ms=d_extend_correlation_ms;
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||||
}else{
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current_synchro_data.correlation_length_ms=1;
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}
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*out[0] = current_synchro_data;
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||||
}else{
|
||||
//todo: fill synchronization data to produce output while coherent integration is running
|
||||
@ -579,10 +580,16 @@ int gps_l1_ca_dll_pll_c_aid_tracking_cc::general_work (int noutput_items, gr_vec
|
||||
current_synchro_data.Tracking_timestamp_secs = (static_cast<double>(d_sample_counter) + d_rem_code_phase_samples) / static_cast<double>(d_fs_in);
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// This tracking block aligns the Tracking_timestamp_secs with the start sample of the PRN, thus, Code_phase_secs=0
|
||||
current_synchro_data.Code_phase_secs = 0;
|
||||
current_synchro_data.Carrier_phase_rads = GPS_TWO_PI * d_acc_carrier_phase_cycles; // todo: project the acc carrier phase
|
||||
current_synchro_data.Carrier_phase_rads = GPS_TWO_PI * d_acc_carrier_phase_cycles;
|
||||
current_synchro_data.Carrier_Doppler_hz = d_carrier_doppler_hz;// todo: project the carrier doppler
|
||||
current_synchro_data.CN0_dB_hz = d_CN0_SNV_dB_Hz;
|
||||
current_synchro_data.Flag_valid_pseudorange = false;
|
||||
if (d_preamble_synchronized==true)
|
||||
{
|
||||
current_synchro_data.correlation_length_ms=d_extend_correlation_ms;
|
||||
}else{
|
||||
current_synchro_data.correlation_length_ms=1;
|
||||
}
|
||||
*out[0] = current_synchro_data;
|
||||
}
|
||||
|
||||
@ -597,7 +604,7 @@ int gps_l1_ca_dll_pll_c_aid_tracking_cc::general_work (int noutput_items, gr_vec
|
||||
{
|
||||
d_last_seg = floor(d_sample_counter / d_fs_in);
|
||||
std::cout << "Current input signal time = " << d_last_seg << " [s]" << std::endl;
|
||||
std::cout << "GPS L1 C/A Tracking CH " << d_channel << ": Satellite " << Gnss_Satellite(systemName[sys], d_acquisition_gnss_synchro->PRN)
|
||||
DLOG(INFO) << "GPS L1 C/A Tracking CH " << d_channel << ": Satellite " << Gnss_Satellite(systemName[sys], d_acquisition_gnss_synchro->PRN)
|
||||
<< ", CN0 = " << d_CN0_SNV_dB_Hz << " [dB-Hz]" << std::endl;
|
||||
//if (d_last_seg==5) d_carrier_lock_fail_counter=500; //DEBUG: force unlock!
|
||||
}
|
||||
@ -607,7 +614,7 @@ int gps_l1_ca_dll_pll_c_aid_tracking_cc::general_work (int noutput_items, gr_vec
|
||||
if (floor(d_sample_counter / d_fs_in) != d_last_seg)
|
||||
{
|
||||
d_last_seg = floor(d_sample_counter / d_fs_in);
|
||||
std::cout << "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]";
|
||||
}
|
||||
}
|
||||
|
@ -74,6 +74,7 @@ const int GPS_L1_CA_HISTORY_DEEP = 100;
|
||||
|
||||
#define GPS_PREAMBLE {1, 0, 0, 0, 1, 0, 1, 1}
|
||||
const int GPS_CA_PREAMBLE_LENGTH_BITS = 8;
|
||||
const int GPS_CA_PREAMBLE_LENGTH_SYMBOLS = 160;
|
||||
const int GPS_CA_TELEMETRY_RATE_BITS_SECOND = 50; //!< NAV message bit rate [bits/s]
|
||||
const int GPS_CA_TELEMETRY_SYMBOLS_PER_BIT = 20;
|
||||
const int GPS_CA_TELEMETRY_RATE_SYMBOLS_SECOND = GPS_CA_TELEMETRY_RATE_BITS_SECOND*20; //!< NAV message bit rate [symbols/s]
|
||||
|
@ -61,7 +61,7 @@ public:
|
||||
double Tracking_timestamp_secs; //!< Set by Tracking processing block
|
||||
bool Flag_valid_tracking;
|
||||
bool Flag_valid_symbol_output;
|
||||
bool symbol_integration_enabled; //!< Set by Tracking processing block
|
||||
int correlation_length_ms; //!< Set by Tracking processing block
|
||||
|
||||
//Telemetry Decoder
|
||||
double Prn_timestamp_ms; //!< Set by Telemetry Decoder processing block
|
||||
|
Loading…
Reference in New Issue
Block a user