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FIX: vtl_data debug_print() method
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@ -54,15 +54,15 @@ void Vtl_Data::init_storage(int n_sats)
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void Vtl_Data::debug_print()
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void Vtl_Data::debug_print()
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{
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{
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std::cout << "vtl_data debug print at RX TOW: " << epoch_tow_s << ", TRK sample counter: " << sample_counter << "\n";
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std::cout << "vtl_data debug print at RX TOW: " << epoch_tow_s << ", TRK sample counter: " << sample_counter << "\n";
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// sat_p.print("VTL Sat Positions");
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sat_p.print("VTL Sat Positions");
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//sat_v.print("VTL Sat Velocities");
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sat_v.print("VTL Sat Velocities");
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// sat_dts.print("VTL Sat clocks");
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sat_dts.print("VTL Sat clocks");
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// sat_var.print("VTL Sat clock variances");
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sat_var.print("VTL Sat clock variances");
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// sat_health_flag.print("VTL Sat health");
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sat_health_flag.print("VTL Sat health");
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//sat_LOS.print("VTL SAT LOS");
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sat_LOS.print("VTL SAT LOS");
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kf_state.print("EKF STATE");
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kf_state.print("EKF STATE");
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//pr_m.print("Satellite Code pseudoranges [m]");
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pr_m.print("Satellite Code pseudoranges [m]");
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//doppler_hz.print("satellite Carrier Dopplers [Hz]");
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doppler_hz.print("satellite Carrier Dopplers [Hz]");
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// carrier_phase_rads.print("satellite accumulated carrier phases [rads]");
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carrier_phase_rads.print("satellite accumulated carrier phases [rad]");
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}
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}
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