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Merge branch 'next' into trk_hi_dyn

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unknown 2018-08-21 22:27:09 +02:00
commit db50655f90
41 changed files with 3195 additions and 112 deletions
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1
AUTHORS
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@ -50,6 +50,7 @@ Daniel Fehr daniel.co@bluewin.ch Contributor
David Pubill david.pubill@cttc.cat Contributor
Fran Fabra fabra@ice.csic.es Contributor
Gabriel Araujo gabriel.araujo.5000@gmail.com Contributor
Gerald LaMountain gerald@gece.neu.edu Contributor
Leonardo Tonetto tonetto.dev@gmail.com Contributor
Mara Branzanti mara.branzanti@gmail.com Contributor
Marc Molina marc.molina.pena@gmail.com Contributor

63
conf/gnss-sdr-kalman-bayes.conf Normal file
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@ -0,0 +1,63 @@
[GNSS-SDR]
;######### GLOBAL OPTIONS ##################
;internal_fs_sps: Internal signal sampling frequency after the signal conditioning stage [samples per second].
GNSS-SDR.internal_fs_sps=2000000
GNSS-SDR.internal_fs_hz=2000000
;######### SIGNAL_SOURCE CONFIG ############
SignalSource.implementation=File_Signal_Source
SignalSource.filename=/home/glamountain/gnss-sdr/data/2013_04_04_GNSS_SIGNAL_at_CTTC_SPAIN/2013_04_04_GNSS_SIGNAL_at_CTTC_SPAIN.dat
SignalSource.item_type=ishort
SignalSource.sampling_frequency=4000000
SignalSource.freq=1575420000
SignalSource.samples=0
;######### SIGNAL_CONDITIONER CONFIG ############
SignalConditioner.implementation=Signal_Conditioner
DataTypeAdapter.implementation=Ishort_To_Complex
InputFilter.implementation=Pass_Through
InputFilter.item_type=gr_complex
Resampler.implementation=Direct_Resampler
Resampler.sample_freq_in=4000000
Resampler.sample_freq_out=2000000
Resampler.item_type=gr_complex
;######### CHANNELS GLOBAL CONFIG ############
Channels_1C.count=8
Channels.in_acquisition=1
Channel.signal=1C
;######### ACQUISITION GLOBAL CONFIG ############
Acquisition_1C.implementation=GPS_L1_CA_PCPS_Acquisition
Acquisition_1C.item_type=gr_complex
Acquisition_1C.threshold=0.008
Acquisition_1C.doppler_max=10000
Acquisition_1C.doppler_step=250
Acquisition_1C.dump=false
Acquisition_1C.dump_filename=../data/kalman/acq_dump
;######### TRACKING GLOBAL CONFIG ############
Tracking_1C.implementation=GPS_L1_CA_KF_Tracking
Tracking_1C.item_type=gr_complex
Tracking_1C.pll_bw_hz=40.0;
Tracking_1C.dll_bw_hz=4.0;
Tracking_1C.order=3;
Tracking_1C.dump=true
Tracking_1C.dump_filename=../data/kalman/epl_tracking_ch_
Tracking_1C.bce_run = true;
Tracking_1C.p_transient = 0;
Tracking_1C.s_transient = 100;
;######### TELEMETRY DECODER GPS CONFIG ############
TelemetryDecoder_1C.implementation=GPS_L1_CA_Telemetry_Decoder
;######### OBSERVABLES CONFIG ############
Observables.implementation=GPS_L1_CA_Observables
;######### PVT CONFIG ############
PVT.implementation=GPS_L1_CA_PVT
PVT.averaging_depth=100
PVT.flag_averaging=true
PVT.output_rate_ms=10
PVT.display_rate_ms=500

211
conf/gnss-sdr_GPS_L1_nsr_kf.conf Normal file
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@ -0,0 +1,211 @@
; Default configuration file
; You can define your own receiver and invoke it by doing
; gnss-sdr --config_file=my_GNSS_SDR_configuration.conf
;
[GNSS-SDR]
;######### GLOBAL OPTIONS ##################
;internal_fs_sps: Internal signal sampling frequency after the signal conditioning stage [samples per second].
;GNSS-SDR.internal_fs_sps=6826700
GNSS-SDR.internal_fs_sps=2560000
;GNSS-SDR.internal_fs_sps=4096000
;GNSS-SDR.internal_fs_sps=5120000
;######### SIGNAL_SOURCE CONFIG ############
;#implementation: Use [File_Signal_Source] [Nsr_File_Signal_Source] or [UHD_Signal_Source] or [GN3S_Signal_Source] (experimental)
SignalSource.implementation=Nsr_File_Signal_Source
;#filename: path to file with the captured GNSS signal samples to be processed
SignalSource.filename=/home/javier/signals/ifen/E1L1_FE0_Band0.stream ; <- PUT YOUR FILE HERE
;#item_type: Type and resolution for each of the signal samples. Use only gr_complex in this version.
SignalSource.item_type=byte
;#sampling_frequency: Original Signal sampling frequency in [Hz]
SignalSource.sampling_frequency=20480000
;#freq: RF front-end center frequency in [Hz]
SignalSource.freq=1575420000
;#samples: Number of samples to be processed. Notice that 0 indicates the entire file.
SignalSource.samples=0
;#repeat: Repeat the processing file. Disable this option in this version
SignalSource.repeat=false
;#dump: Dump the Signal source data to a file. Disable this option in this version
SignalSource.dump=false
SignalSource.dump_filename=../data/signal_source.dat
;#enable_throttle_control: Enabling this option tells the signal source to keep the delay between samples in post processing.
; it helps to not overload the CPU, but the processing time will be longer.
SignalSource.enable_throttle_control=false
;######### SIGNAL_CONDITIONER CONFIG ############
;## It holds blocks to change data type, filter and resample input data.
;#implementation: Use [Pass_Through] or [Signal_Conditioner]
;#[Pass_Through] disables this block and the [DataTypeAdapter], [InputFilter] and [Resampler] blocks
;#[Signal_Conditioner] enables this block. Then you have to configure [DataTypeAdapter], [InputFilter] and [Resampler] blocks
SignalConditioner.implementation=Signal_Conditioner
;######### DATA_TYPE_ADAPTER CONFIG ############
;## Changes the type of input data.
;#implementation: [Pass_Through] disables this block
DataTypeAdapter.implementation=Pass_Through
DataTypeAdapter.item_type=float
;######### INPUT_FILTER CONFIG ############
;## Filter the input data. Can be combined with frequency translation for IF signals
;#implementation: Use [Pass_Through] or [Fir_Filter] or [Freq_Xlating_Fir_Filter]
;#[Freq_Xlating_Fir_Filter] enables FIR filter and a composite frequency translation
;# that shifts IF down to zero Hz.
InputFilter.implementation=Freq_Xlating_Fir_Filter
;#dump: Dump the filtered data to a file.
InputFilter.dump=false
;#dump_filename: Log path and filename.
InputFilter.dump_filename=../data/input_filter.dat
;#The following options are used in the filter design of Fir_Filter and Freq_Xlating_Fir_Filter implementation.
;#These options are based on parameters of gnuradio's function: gr_remez.
;#These function calculates the optimal (in the Chebyshev/minimax sense) FIR filter inpulse
;#reponse given a set of band edges, the desired reponse on those bands,
;#and the weight given to the error in those bands.
;#input_item_type: Type and resolution for input signal samples. Use only gr_complex in this version.
InputFilter.input_item_type=float
;#outut_item_type: Type and resolution for output filtered signal samples. Use only gr_complex in this version.
InputFilter.output_item_type=gr_complex
;#taps_item_type: Type and resolution for the taps of the filter. Use only float in this version.
InputFilter.taps_item_type=float
;#number_of_taps: Number of taps in the filter. Increasing this parameter increases the processing time
InputFilter.number_of_taps=5
;#number_of _bands: Number of frequency bands in the filter.
InputFilter.number_of_bands=2
;#bands: frequency at the band edges [ b1 e1 b2 e2 b3 e3 ...].
;#Frequency is in the range [0, 1], with 1 being the Nyquist frequency (Fs/2)
;#The number of band_begin and band_end elements must match the number of bands
InputFilter.band1_begin=0.0
InputFilter.band1_end=0.45
InputFilter.band2_begin=0.55
InputFilter.band2_end=1.0
;#ampl: desired amplitude at the band edges [ a(b1) a(e1) a(b2) a(e2) ...].
;#The number of ampl_begin and ampl_end elements must match the number of bands
InputFilter.ampl1_begin=1.0
InputFilter.ampl1_end=1.0
InputFilter.ampl2_begin=0.0
InputFilter.ampl2_end=0.0
;#band_error: weighting applied to each band (usually 1).
;#The number of band_error elements must match the number of bands
InputFilter.band1_error=1.0
InputFilter.band2_error=1.0
;#filter_type: one of "bandpass", "hilbert" or "differentiator"
InputFilter.filter_type=bandpass
;#grid_density: determines how accurately the filter will be constructed.
;The minimum value is 16; higher values are slower to compute the filter.
InputFilter.grid_density=16
;# Original sampling frequency stored in the signal file
InputFilter.sampling_frequency=20480000
;#The following options are used only in Freq_Xlating_Fir_Filter implementation.
;#InputFilter.IF is the intermediate frequency (in Hz) shifted down to zero Hz
InputFilter.IF=5499998.47412109
;# Decimation factor after the frequency tranaslating block
InputFilter.decimation_factor=8
;######### RESAMPLER CONFIG ############
;## Resamples the input data.
;#implementation: Use [Pass_Through] or [Direct_Resampler]
;#[Pass_Through] disables this block
;#[Direct_Resampler] enables a resampler that implements a nearest neigbourhood interpolation
Resampler.implementation=Pass_Through
;######### CHANNELS GLOBAL CONFIG ############
;#count: Number of available GPS satellite channels.
Channels_1C.count=8
Channels.in_acquisition=1
#Channel.signal=1C
;######### ACQUISITION GLOBAL CONFIG ############
Acquisition_1C.dump=false
Acquisition_1C.dump_filename=./acq_dump.dat
Acquisition_1C.item_type=gr_complex
Acquisition_1C.if=0
Acquisition_1C.sampled_ms=1
Acquisition_1C.implementation=GPS_L1_CA_PCPS_Acquisition
;#use_CFAR_algorithm: If enabled, acquisition estimates the input signal power to implement CFAR detection algorithms
;#notice that this affects the Acquisition threshold range!
Acquisition_1C.use_CFAR_algorithm=false;
;#threshold: Acquisition threshold
Acquisition_1C.threshold=10
;Acquisition_1C.pfa=0.01
Acquisition_1C.doppler_max=5000
Acquisition_1C.doppler_step=100
;######### TRACKING GPS CONFIG ############
Tracking_1C.implementation=GPS_L1_CA_KF_Tracking
Tracking_1C.item_type=gr_complex
Tracking_1C.if=0
Tracking_1C.dump=true
Tracking_1C.dump_filename=../data/epl_tracking_ch_
Tracking_1C.pll_bw_hz=15.0;
Tracking_1C.dll_bw_hz=2.0;
Tracking_1C.order=3;
;######### TELEMETRY DECODER GPS CONFIG ############
TelemetryDecoder_1C.implementation=GPS_L1_CA_Telemetry_Decoder
TelemetryDecoder_1C.dump=false
TelemetryDecoder_1C.decimation_factor=1;
;######### OBSERVABLES CONFIG ############
;#implementation:
Observables.implementation=Hybrid_Observables
;#dump: Enable or disable the Observables internal binary data file logging [true] or [false]
Observables.dump=false
;#dump_filename: Log path and filename.
Observables.dump_filename=./observables.dat
;######### PVT CONFIG ############
PVT.implementation=RTKLIB_PVT
PVT.positioning_mode=PPP_Static ; options: Single, Static, Kinematic, PPP_Static, PPP_Kinematic
PVT.iono_model=Broadcast ; options: OFF, Broadcast, SBAS, Iono-Free-LC, Estimate_STEC, IONEX
PVT.trop_model=Saastamoinen ; options: OFF, Saastamoinen, SBAS, Estimate_ZTD, Estimate_ZTD_Grad
PVT.output_rate_ms=100
PVT.display_rate_ms=500
PVT.dump_filename=./PVT
PVT.nmea_dump_filename=./gnss_sdr_pvt.nmea;
PVT.flag_nmea_tty_port=false;
PVT.nmea_dump_devname=/dev/pts/4
PVT.flag_rtcm_server=false
PVT.flag_rtcm_tty_port=false
PVT.rtcm_dump_devname=/dev/pts/1
PVT.dump=true

11
src/algorithms/acquisition/gnuradio_blocks/galileo_e5a_noncoherent_iq_acquisition_caf_cc.cc
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@ -280,7 +280,8 @@ void galileo_e5a_noncoherentIQ_acquisition_caf_cc::init()
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_doppler_step = 0U;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_mag = 0.0;
d_input_power = 0.0;
const double GALILEO_TWO_PI = 6.283185307179600;
@ -328,7 +329,8 @@ void galileo_e5a_noncoherentIQ_acquisition_caf_cc::set_state(int state)
{
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_well_count = 0;
d_mag = 0.0;
d_input_power = 0.0;
@ -376,7 +378,8 @@ int galileo_e5a_noncoherentIQ_acquisition_caf_cc::general_work(int noutput_items
//restart acquisition variables
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_well_count = 0;
d_mag = 0.0;
d_input_power = 0.0;
@ -633,7 +636,7 @@ int galileo_e5a_noncoherentIQ_acquisition_caf_cc::general_work(int noutput_items
d_gnss_synchro->Acq_delay_samples = static_cast<double>(indext % d_samples_per_code);
d_gnss_synchro->Acq_doppler_hz = static_cast<double>(doppler);
d_gnss_synchro->Acq_samplestamp_samples = d_sample_counter;
d_gnss_synchro->Acq_doppler_step = d_doppler_step;
// 5- Compute the test statistics and compare to the threshold
d_test_statistics = d_mag / d_input_power;
}

11
src/algorithms/acquisition/gnuradio_blocks/galileo_pcps_8ms_acquisition_cc.cc
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@ -151,10 +151,10 @@ void galileo_pcps_8ms_acquisition_cc::init()
d_gnss_synchro->Flag_valid_symbol_output = false;
d_gnss_synchro->Flag_valid_pseudorange = false;
d_gnss_synchro->Flag_valid_word = false;
d_gnss_synchro->Acq_doppler_step = 0U;
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_mag = 0.0;
d_input_power = 0.0;
const double GALILEO_TWO_PI = 6.283185307179600;
@ -188,7 +188,8 @@ void galileo_pcps_8ms_acquisition_cc::set_state(int state)
{
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_well_count = 0;
d_mag = 0.0;
d_input_power = 0.0;
@ -219,7 +220,8 @@ int galileo_pcps_8ms_acquisition_cc::general_work(int noutput_items,
//restart acquisition variables
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_well_count = 0;
d_mag = 0.0;
d_input_power = 0.0;
@ -328,6 +330,7 @@ int galileo_pcps_8ms_acquisition_cc::general_work(int noutput_items,
d_gnss_synchro->Acq_delay_samples = static_cast<double>(indext % d_samples_per_code);
d_gnss_synchro->Acq_doppler_hz = static_cast<double>(doppler);
d_gnss_synchro->Acq_samplestamp_samples = d_sample_counter;
d_gnss_synchro->Acq_doppler_step = d_doppler_step;
}
// Record results to file if required

5
src/algorithms/acquisition/gnuradio_blocks/pcps_acquisition.cc
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@ -261,7 +261,7 @@ void pcps_acquisition::init()
d_gnss_synchro->Flag_valid_symbol_output = false;
d_gnss_synchro->Flag_valid_pseudorange = false;
d_gnss_synchro->Flag_valid_word = false;
d_gnss_synchro->Acq_doppler_step = 0U;
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
@ -334,6 +334,7 @@ void pcps_acquisition::set_state(int32_t state)
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_mag = 0.0;
d_input_power = 0.0;
d_test_statistics = 0.0;
@ -725,6 +726,7 @@ void pcps_acquisition::acquisition_core(uint64_t samp_count)
d_gnss_synchro->Acq_delay_samples = static_cast<double>(std::fmod(static_cast<float>(indext), acq_parameters.samples_per_code));
d_gnss_synchro->Acq_doppler_hz = static_cast<double>(doppler);
d_gnss_synchro->Acq_samplestamp_samples = samp_count;
d_gnss_synchro->Acq_doppler_step = acq_parameters.doppler_step2;
}
lk.lock();
@ -865,6 +867,7 @@ int pcps_acquisition::general_work(int noutput_items __attribute__((unused)),
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_mag = 0.0;
d_input_power = 0.0;
d_test_statistics = 0.0;

8
src/algorithms/acquisition/gnuradio_blocks/pcps_acquisition_fine_doppler_cc.cc
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@ -180,10 +180,10 @@ void pcps_acquisition_fine_doppler_cc::init()
d_gnss_synchro->Flag_valid_symbol_output = false;
d_gnss_synchro->Flag_valid_pseudorange = false;
d_gnss_synchro->Flag_valid_word = false;
d_gnss_synchro->Acq_doppler_step = 0U;
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_state = 0;
}
@ -295,6 +295,7 @@ double pcps_acquisition_fine_doppler_cc::compute_CAF()
d_gnss_synchro->Acq_delay_samples = static_cast<double>(index_time);
d_gnss_synchro->Acq_doppler_hz = static_cast<double>(index_doppler * d_doppler_step - d_config_doppler_max);
d_gnss_synchro->Acq_samplestamp_samples = d_sample_counter;
d_gnss_synchro->Acq_doppler_step = d_doppler_step;
return d_test_statistics;
}
@ -461,7 +462,8 @@ void pcps_acquisition_fine_doppler_cc::set_state(int state)
{
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_well_count = 0;
d_test_statistics = 0.0;
d_active = true;

5
src/algorithms/acquisition/gnuradio_blocks/pcps_assisted_acquisition_cc.cc
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@ -150,10 +150,10 @@ void pcps_assisted_acquisition_cc::init()
d_gnss_synchro->Flag_valid_symbol_output = false;
d_gnss_synchro->Flag_valid_pseudorange = false;
d_gnss_synchro->Flag_valid_word = false;
d_gnss_synchro->Acq_doppler_step = 0U;
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_input_power = 0.0;
d_state = 0;
@ -279,6 +279,7 @@ double pcps_assisted_acquisition_cc::search_maximum()
d_gnss_synchro->Acq_delay_samples = static_cast<double>(index_time);
d_gnss_synchro->Acq_doppler_hz = static_cast<double>(index_doppler * d_doppler_step + d_doppler_min);
d_gnss_synchro->Acq_samplestamp_samples = d_sample_counter;
d_gnss_synchro->Acq_doppler_step = d_doppler_step;
// Record results to file if required
if (d_dump)

11
src/algorithms/acquisition/gnuradio_blocks/pcps_cccwsr_acquisition_cc.cc
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@ -165,10 +165,10 @@ void pcps_cccwsr_acquisition_cc::init()
d_gnss_synchro->Flag_valid_symbol_output = false;
d_gnss_synchro->Flag_valid_pseudorange = false;
d_gnss_synchro->Flag_valid_word = false;
d_gnss_synchro->Acq_doppler_step = 0U;
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_mag = 0.0;
d_input_power = 0.0;
@ -203,7 +203,8 @@ void pcps_cccwsr_acquisition_cc::set_state(int state)
{
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_well_count = 0;
d_mag = 0.0;
d_input_power = 0.0;
@ -234,7 +235,8 @@ int pcps_cccwsr_acquisition_cc::general_work(int noutput_items,
//restart acquisition variables
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_well_count = 0;
d_mag = 0.0;
d_input_power = 0.0;
@ -354,6 +356,7 @@ int pcps_cccwsr_acquisition_cc::general_work(int noutput_items,
d_gnss_synchro->Acq_delay_samples = static_cast<double>(indext % d_samples_per_code);
d_gnss_synchro->Acq_doppler_hz = static_cast<double>(doppler);
d_gnss_synchro->Acq_samplestamp_samples = d_sample_counter;
d_gnss_synchro->Acq_doppler_step = d_doppler_step;
}
// Record results to file if required

12
src/algorithms/acquisition/gnuradio_blocks/pcps_opencl_acquisition_cc.cc
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@ -290,10 +290,10 @@ void pcps_opencl_acquisition_cc::init()
d_gnss_synchro->Flag_valid_symbol_output = false;
d_gnss_synchro->Flag_valid_pseudorange = false;
d_gnss_synchro->Flag_valid_word = false;
d_gnss_synchro->Acq_doppler_step = 0U;
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_mag = 0.0;
d_input_power = 0.0;
@ -450,6 +450,7 @@ void pcps_opencl_acquisition_cc::acquisition_core_volk()
d_gnss_synchro->Acq_delay_samples = static_cast<double>(indext % d_samples_per_code);
d_gnss_synchro->Acq_doppler_hz = static_cast<double>(doppler);
d_gnss_synchro->Acq_samplestamp_samples = samplestamp;
d_gnss_synchro->Acq_doppler_step = d_doppler_step;
// 5- Compute the test statistics and compare to the threshold
//d_test_statistics = 2 * d_fft_size * d_mag / d_input_power;
@ -613,6 +614,7 @@ void pcps_opencl_acquisition_cc::acquisition_core_opencl()
d_gnss_synchro->Acq_delay_samples = static_cast<double>(indext % d_samples_per_code);
d_gnss_synchro->Acq_doppler_hz = static_cast<double>(doppler);
d_gnss_synchro->Acq_samplestamp_samples = samplestamp;
d_gnss_synchro->Acq_doppler_step = d_doppler_step;
// 5- Compute the test statistics and compare to the threshold
//d_test_statistics = 2 * d_fft_size * d_mag / d_input_power;
@ -676,7 +678,8 @@ void pcps_opencl_acquisition_cc::set_state(int state)
{
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_well_count = 0;
d_mag = 0.0;
d_input_power = 0.0;
@ -708,7 +711,8 @@ int pcps_opencl_acquisition_cc::general_work(int noutput_items,
//restart acquisition variables
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_well_count = 0;
d_mag = 0.0;
d_input_power = 0.0;

10
src/algorithms/acquisition/gnuradio_blocks/pcps_quicksync_acquisition_cc.cc
View File

@ -199,7 +199,8 @@ void pcps_quicksync_acquisition_cc::init()
//DLOG(INFO) << "START init";
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_mag = 0.0;
d_input_power = 0.0;
@ -236,7 +237,8 @@ void pcps_quicksync_acquisition_cc::set_state(int state)
{
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_well_count = 0;
d_mag = 0.0;
d_input_power = 0.0;
@ -279,7 +281,8 @@ int pcps_quicksync_acquisition_cc::general_work(int noutput_items,
//restart acquisition variables
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_well_count = 0;
d_mag = 0.0;
d_input_power = 0.0;
@ -456,6 +459,7 @@ int pcps_quicksync_acquisition_cc::general_work(int noutput_items,
d_gnss_synchro->Acq_delay_samples = static_cast<double>(d_possible_delay[indext]);
d_gnss_synchro->Acq_doppler_hz = static_cast<double>(doppler);
d_gnss_synchro->Acq_samplestamp_samples = d_sample_counter;
d_gnss_synchro->Acq_doppler_step = d_doppler_step;
/* 5- Compute the test statistics and compare to the threshold d_test_statistics = 2 * d_fft_size * d_mag / d_input_power;*/
d_test_statistics = d_mag / d_input_power;

11
src/algorithms/acquisition/gnuradio_blocks/pcps_tong_acquisition_cc.cc
View File

@ -166,10 +166,10 @@ void pcps_tong_acquisition_cc::init()
d_gnss_synchro->Flag_valid_symbol_output = false;
d_gnss_synchro->Flag_valid_pseudorange = false;
d_gnss_synchro->Flag_valid_word = false;
d_gnss_synchro->Acq_doppler_step = 0U;
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_mag = 0.0;
d_input_power = 0.0;
@ -211,7 +211,8 @@ void pcps_tong_acquisition_cc::set_state(int state)
{
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_dwell_count = 0;
d_tong_count = d_tong_init_val;
d_mag = 0.0;
@ -250,7 +251,8 @@ int pcps_tong_acquisition_cc::general_work(int noutput_items,
//restart acquisition variables
d_gnss_synchro->Acq_delay_samples = 0.0;
d_gnss_synchro->Acq_doppler_hz = 0.0;
d_gnss_synchro->Acq_samplestamp_samples = 0;
d_gnss_synchro->Acq_samplestamp_samples = 0ULL;
d_gnss_synchro->Acq_doppler_step = 0U;
d_dwell_count = 0;
d_tong_count = d_tong_init_val;
d_mag = 0.0;
@ -345,6 +347,7 @@ int pcps_tong_acquisition_cc::general_work(int noutput_items,
d_gnss_synchro->Acq_delay_samples = static_cast<double>(indext % d_samples_per_code);
d_gnss_synchro->Acq_doppler_hz = static_cast<double>(doppler);
d_gnss_synchro->Acq_samplestamp_samples = d_sample_counter;
d_gnss_synchro->Acq_doppler_step = d_doppler_step;
}
// Record results to file if required

10
src/algorithms/telemetry_decoder/gnuradio_blocks/galileo_e1b_telemetry_decoder_cc.cc
View File

@ -314,7 +314,7 @@ int galileo_e1b_telemetry_decoder_cc::general_work(int noutput_items __attribute
consume_each(1);
d_flag_preamble = false;
uint32_t required_symbols = GALILEO_INAV_PAGE_SYMBOLS + d_symbols_per_preamble;
uint32_t required_symbols = static_cast<uint32_t>(GALILEO_INAV_PAGE_SYMBOLS) + static_cast<uint32_t>(d_symbols_per_preamble);
if (d_symbol_history.size() > required_symbols)
{
@ -427,7 +427,7 @@ int galileo_e1b_telemetry_decoder_cc::general_work(int noutput_items __attribute
{
// TOW_5 refers to the even preamble, but when we decode it we are in the odd part, so 1 second later plus the decoding delay
d_TOW_at_Preamble_ms = static_cast<uint32_t>(d_nav.TOW_5 * 1000.0);
d_TOW_at_current_symbol_ms = d_TOW_at_Preamble_ms + GALILEO_INAV_PAGE_PART_MS + (required_symbols + 1) * GALILEO_E1_CODE_PERIOD_MS;
d_TOW_at_current_symbol_ms = d_TOW_at_Preamble_ms + static_cast<uint32_t>(GALILEO_INAV_PAGE_PART_MS + (required_symbols + 1) * GALILEO_E1_CODE_PERIOD_MS);
d_nav.flag_TOW_5 = false;
}
@ -435,20 +435,20 @@ int galileo_e1b_telemetry_decoder_cc::general_work(int noutput_items __attribute
{
// TOW_6 refers to the even preamble, but when we decode it we are in the odd part, so 1 second later plus the decoding delay
d_TOW_at_Preamble_ms = static_cast<uint32_t>(d_nav.TOW_6 * 1000.0);
d_TOW_at_current_symbol_ms = d_TOW_at_Preamble_ms + GALILEO_INAV_PAGE_PART_MS + (required_symbols + 1) * GALILEO_E1_CODE_PERIOD_MS;
d_TOW_at_current_symbol_ms = d_TOW_at_Preamble_ms + static_cast<uint32_t>(GALILEO_INAV_PAGE_PART_MS + (required_symbols + 1) * GALILEO_E1_CODE_PERIOD_MS);
d_nav.flag_TOW_6 = false;
}
else
{
// this page has no timing information
d_TOW_at_current_symbol_ms += GALILEO_E1_CODE_PERIOD_MS; // + GALILEO_INAV_PAGE_PART_SYMBOLS*GALILEO_E1_CODE_PERIOD;
d_TOW_at_current_symbol_ms += static_cast<uint32_t>(GALILEO_E1_CODE_PERIOD_MS); // + GALILEO_INAV_PAGE_PART_SYMBOLS*GALILEO_E1_CODE_PERIOD;
}
}
else // if there is not a new preamble, we define the TOW of the current symbol
{
if (d_nav.flag_TOW_set == true)
{
d_TOW_at_current_symbol_ms += GALILEO_E1_CODE_PERIOD_MS;
d_TOW_at_current_symbol_ms += static_cast<uint32_t>(GALILEO_E1_CODE_PERIOD_MS);
}
}

12
src/algorithms/telemetry_decoder/gnuradio_blocks/galileo_e5a_telemetry_decoder_cc.cc
View File

@ -438,37 +438,37 @@ int galileo_e5a_telemetry_decoder_cc::general_work(int noutput_items __attribute
if (d_nav.flag_TOW_1 == true)
{
d_TOW_at_Preamble_ms = static_cast<uint32_t>(d_nav.FNAV_TOW_1 * 1000.0);
d_TOW_at_current_symbol_ms = d_TOW_at_Preamble_ms + (GALILEO_FNAV_CODES_PER_PAGE + GALILEO_FNAV_CODES_PER_PREAMBLE) * GALILEO_E5a_CODE_PERIOD_MS;
d_TOW_at_current_symbol_ms = d_TOW_at_Preamble_ms + static_cast<uint32_t>((GALILEO_FNAV_CODES_PER_PAGE + GALILEO_FNAV_CODES_PER_PREAMBLE) * GALILEO_E5a_CODE_PERIOD_MS);
d_nav.flag_TOW_1 = false;
}
else if (d_nav.flag_TOW_2 == true)
{
d_TOW_at_Preamble_ms = static_cast<uint32_t>(d_nav.FNAV_TOW_2 * 1000.0);
d_TOW_at_current_symbol_ms = d_TOW_at_Preamble_ms + (GALILEO_FNAV_CODES_PER_PAGE + GALILEO_FNAV_CODES_PER_PREAMBLE) * GALILEO_E5a_CODE_PERIOD_MS;
d_TOW_at_current_symbol_ms = d_TOW_at_Preamble_ms + static_cast<uint32_t>((GALILEO_FNAV_CODES_PER_PAGE + GALILEO_FNAV_CODES_PER_PREAMBLE) * GALILEO_E5a_CODE_PERIOD_MS);
d_nav.flag_TOW_2 = false;
}
else if (d_nav.flag_TOW_3 == true)
{
d_TOW_at_Preamble_ms = static_cast<uint32_t>(d_nav.FNAV_TOW_3 * 1000.0);
d_TOW_at_current_symbol_ms = d_TOW_at_Preamble_ms + (GALILEO_FNAV_CODES_PER_PAGE + GALILEO_FNAV_CODES_PER_PREAMBLE) * GALILEO_E5a_CODE_PERIOD_MS;
d_TOW_at_current_symbol_ms = d_TOW_at_Preamble_ms + static_cast<uint32_t>((GALILEO_FNAV_CODES_PER_PAGE + GALILEO_FNAV_CODES_PER_PREAMBLE) * GALILEO_E5a_CODE_PERIOD_MS);
d_nav.flag_TOW_3 = false;
}
else if (d_nav.flag_TOW_4 == true)
{
d_TOW_at_Preamble_ms = static_cast<uint32_t>(d_nav.FNAV_TOW_4 * 1000.0);
d_TOW_at_current_symbol_ms = d_TOW_at_Preamble_ms + (GALILEO_FNAV_CODES_PER_PAGE + GALILEO_FNAV_CODES_PER_PREAMBLE) * GALILEO_E5a_CODE_PERIOD_MS;
d_TOW_at_current_symbol_ms = d_TOW_at_Preamble_ms + static_cast<uint32_t>((GALILEO_FNAV_CODES_PER_PAGE + GALILEO_FNAV_CODES_PER_PREAMBLE) * GALILEO_E5a_CODE_PERIOD_MS);
d_nav.flag_TOW_4 = false;
}
else
{
d_TOW_at_current_symbol_ms += GALILEO_E5a_CODE_PERIOD_MS;
d_TOW_at_current_symbol_ms += static_cast<uint32_t>(GALILEO_E5a_CODE_PERIOD_MS);
}
}
else // if there is not a new preamble, we define the TOW of the current symbol
{
if (d_nav.flag_TOW_set == true)
{
d_TOW_at_current_symbol_ms += GALILEO_E5a_CODE_PERIOD_MS;
d_TOW_at_current_symbol_ms += static_cast<uint32_t>(GALILEO_E5a_CODE_PERIOD_MS);
}
}

24
src/algorithms/telemetry_decoder/gnuradio_blocks/gps_l1_ca_telemetry_decoder_cc.cc
View File

@ -82,7 +82,7 @@ gps_l1_ca_telemetry_decoder_cc::gps_l1_ca_telemetry_decoder_cc(
n++;
}
}
d_stat = 0;
d_stat = 0U;
d_flag_frame_sync = false;
d_prev_GPS_frame_4bytes = 0;
d_TOW_at_Preamble_ms = 0;
@ -93,8 +93,7 @@ gps_l1_ca_telemetry_decoder_cc::gps_l1_ca_telemetry_decoder_cc(
flag_PLL_180_deg_phase_locked = false;
d_preamble_time_samples = 0ULL;
d_TOW_at_current_symbol_ms = 0;
d_symbol_history.resize(GPS_CA_PREAMBLE_LENGTH_SYMBOLS); // Change fixed buffer size
d_symbol_history.clear(); // Clear all the elements in the buffer
d_symbol_history.set_capacity(GPS_CA_PREAMBLE_LENGTH_SYMBOLS);
d_crc_error_synchronization_counter = 0;
d_current_subframe_symbol = 0;
}
@ -103,6 +102,7 @@ gps_l1_ca_telemetry_decoder_cc::gps_l1_ca_telemetry_decoder_cc(
gps_l1_ca_telemetry_decoder_cc::~gps_l1_ca_telemetry_decoder_cc()
{
volk_gnsssdr_free(d_preambles_symbols);
d_symbol_history.clear();
if (d_dump_file.is_open() == true)
{
try
@ -321,7 +321,7 @@ int gps_l1_ca_telemetry_decoder_cc::general_work(int noutput_items __attribute__
// record the oldest subframe symbol before inserting a new symbol into the circular buffer
if (d_current_subframe_symbol < GPS_SUBFRAME_MS and d_symbol_history.size() > 0)
{
d_subframe_symbols[d_current_subframe_symbol] = d_symbol_history.at(0).Prompt_I;
d_subframe_symbols[d_current_subframe_symbol] = d_symbol_history[0].Prompt_I;
d_current_subframe_symbol++;
}
@ -337,9 +337,9 @@ int gps_l1_ca_telemetry_decoder_cc::general_work(int noutput_items __attribute__
// std::cout << "-------\n";
for (uint32_t i = 0; i < GPS_CA_PREAMBLE_LENGTH_SYMBOLS; i++)
{
if (d_symbol_history.at(i).Flag_valid_symbol_output == true)
if (d_symbol_history[i].Flag_valid_symbol_output == true)
{
if (d_symbol_history.at(i).Prompt_I < 0) // symbols clipping
if (d_symbol_history[i].Prompt_I < 0) // symbols clipping
{
corr_value -= d_preambles_symbols[i];
}
@ -358,18 +358,18 @@ int gps_l1_ca_telemetry_decoder_cc::general_work(int noutput_items __attribute__
if (d_stat == 0)
{
// record the preamble sample stamp
d_preamble_time_samples = d_symbol_history.at(0).Tracking_sample_counter; // record the preamble sample stamp
DLOG(INFO) << "Preamble detection for SAT " << this->d_satellite << "d_symbol_history.at(0).Tracking_sample_counter=" << d_symbol_history.at(0).Tracking_sample_counter;
d_preamble_time_samples = d_symbol_history[0].Tracking_sample_counter; // record the preamble sample stamp
DLOG(INFO) << "Preamble detection for SAT " << this->d_satellite << "d_symbol_history[0].Tracking_sample_counter=" << d_symbol_history[0].Tracking_sample_counter;
d_stat = 1; // enter into frame pre-detection status
}
else if (d_stat == 1) // check 6 seconds of preamble separation
{
preamble_diff_ms = std::round(((static_cast<double>(d_symbol_history.at(0).Tracking_sample_counter) - static_cast<double>(d_preamble_time_samples)) / static_cast<double>(d_symbol_history.at(0).fs)) * 1000.0);
preamble_diff_ms = std::round(((static_cast<double>(d_symbol_history[0].Tracking_sample_counter) - static_cast<double>(d_preamble_time_samples)) / static_cast<double>(d_symbol_history[0].fs)) * 1000.0);
if (std::abs(preamble_diff_ms - GPS_SUBFRAME_MS) % GPS_SUBFRAME_MS == 0)
{
DLOG(INFO) << "Preamble confirmation for SAT " << this->d_satellite;
d_flag_preamble = true;
d_preamble_time_samples = d_symbol_history.at(0).Tracking_sample_counter; // record the PRN start sample index associated to the preamble
d_preamble_time_samples = d_symbol_history[0].Tracking_sample_counter; // record the PRN start sample index associated to the preamble
if (!d_flag_frame_sync)
{
d_flag_frame_sync = true;
@ -383,7 +383,7 @@ int gps_l1_ca_telemetry_decoder_cc::general_work(int noutput_items __attribute__
flag_PLL_180_deg_phase_locked = false;
}
DLOG(INFO) << " Frame sync SAT " << this->d_satellite << " with preamble start at "
<< static_cast<double>(d_preamble_time_samples) / static_cast<double>(d_symbol_history.at(0).fs) << " [s]";
<< static_cast<double>(d_preamble_time_samples) / static_cast<double>(d_symbol_history[0].fs) << " [s]";
}
// try to decode the subframe:
@ -407,7 +407,7 @@ int gps_l1_ca_telemetry_decoder_cc::general_work(int noutput_items __attribute__
{
if (d_stat == 1)
{
preamble_diff_ms = round(((static_cast<double>(d_symbol_history.at(0).Tracking_sample_counter) - static_cast<double>(d_preamble_time_samples)) / static_cast<double>(d_symbol_history.at(0).fs)) * 1000.0);
preamble_diff_ms = round(((static_cast<double>(d_symbol_history[0].Tracking_sample_counter) - static_cast<double>(d_preamble_time_samples)) / static_cast<double>(d_symbol_history[0].fs)) * 1000.0);
if (preamble_diff_ms > GPS_SUBFRAME_MS)
{
DLOG(INFO) << "Lost of frame sync SAT " << this->d_satellite << " preamble_diff= " << preamble_diff_ms;

4
src/algorithms/telemetry_decoder/gnuradio_blocks/gps_l5_telemetry_decoder_cc.cc
View File

@ -64,8 +64,8 @@ gps_l5_telemetry_decoder_cc::gps_l5_telemetry_decoder_cc(
DLOG(INFO) << "GPS L5 TELEMETRY PROCESSING: satellite " << d_satellite;
d_channel = 0;
d_flag_valid_word = false;
d_TOW_at_current_symbol_ms = 0;
d_TOW_at_Preamble_ms = 0;
d_TOW_at_current_symbol_ms = 0U;
d_TOW_at_Preamble_ms = 0U;
// initialize the CNAV frame decoder (libswiftcnav)
cnav_msg_decoder_init(&d_cnav_decoder);
for (int32_t aux = 0; aux < GPS_L5i_NH_CODE_LENGTH; aux++)

2
src/algorithms/tracking/adapters/CMakeLists.txt
View File

@ -35,6 +35,7 @@ set(TRACKING_ADAPTER_SOURCES
gps_l2_m_dll_pll_tracking.cc
glonass_l1_ca_dll_pll_tracking.cc
glonass_l1_ca_dll_pll_c_aid_tracking.cc
gps_l1_ca_kf_tracking.cc
gps_l5_dll_pll_tracking.cc
glonass_l2_ca_dll_pll_tracking.cc
glonass_l2_ca_dll_pll_c_aid_tracking.cc
@ -49,6 +50,7 @@ include_directories(
${CMAKE_SOURCE_DIR}/src/algorithms/tracking/gnuradio_blocks
${CMAKE_SOURCE_DIR}/src/algorithms/tracking/libs
${CMAKE_SOURCE_DIR}/src/algorithms/libs
${ARMADILLO_INCLUDE_DIRS}
${GLOG_INCLUDE_DIRS}
${GFlags_INCLUDE_DIRS}
${GNURADIO_RUNTIME_INCLUDE_DIRS}

174
src/algorithms/tracking/adapters/gps_l1_ca_kf_tracking.cc Normal file
View File

@ -0,0 +1,174 @@
/*!
* \file gps_l1_ca_kf_tracking.cc
* \brief Implementation of an adapter of a DLL + Kalman carrier
* tracking loop block for GPS L1 C/A signals
* \author Javier Arribas, 2018. jarribas(at)cttc.es
* \author Jordi Vila-Valls 2018. jvila(at)cttc.es
* \author Carles Fernandez-Prades 2018. cfernandez(at)cttc.es
*
* Reference:
* J. Vila-Valls, P. Closas, M. Navarro and C. Fernández-Prades,
* "Are PLLs Dead? A Tutorial on Kalman Filter-based Techniques for Digital
* Carrier Synchronization", IEEE Aerospace and Electronic Systems Magazine,
* Vol. 32, No. 7, pp. 28–45, July 2017. DOI: 10.1109/MAES.2017.150260
*
* -------------------------------------------------------------------------
*
* Copyright (C) 2010-2018 (see AUTHORS file for a list of contributors)
*
* GNSS-SDR is a software defined Global Navigation
* Satellite Systems receiver
*
* This file is part of GNSS-SDR.
*
* GNSS-SDR is free software: you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation, either version 3 of the License, or
* (at your option) any later version.
*
* GNSS-SDR is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with GNSS-SDR. If not, see <http://www.gnu.org/licenses/>.
*
* -------------------------------------------------------------------------
*/
#include "gps_l1_ca_kf_tracking.h"
#include "gnss_sdr_flags.h"
#include "GPS_L1_CA.h"
#include "configuration_interface.h"
#include <glog/logging.h>
using google::LogMessage;
GpsL1CaKfTracking::GpsL1CaKfTracking(
ConfigurationInterface* configuration, std::string role,
unsigned int in_streams, unsigned int out_streams) : role_(role), in_streams_(in_streams), out_streams_(out_streams)
{
DLOG(INFO) << "role " << role;
//################# CONFIGURATION PARAMETERS ########################
int order;
int fs_in;
int vector_length;
int f_if;
bool dump;
std::string dump_filename;
std::string item_type;
std::string default_item_type = "gr_complex";
float dll_bw_hz;
float early_late_space_chips;
bool bce_run;
unsigned int bce_ptrans;
unsigned int bce_strans;
int bce_nu;
int bce_kappa;
item_type = configuration->property(role + ".item_type", default_item_type);
order = configuration->property(role + ".order", 2);
int fs_in_deprecated = configuration->property("GNSS-SDR.internal_fs_hz", 2048000);
fs_in = configuration->property("GNSS-SDR.internal_fs_sps", fs_in_deprecated);
f_if = configuration->property(role + ".if", 0);
dump = configuration->property(role + ".dump", false);
dll_bw_hz = configuration->property(role + ".dll_bw_hz", 2.0);
if (FLAGS_dll_bw_hz != 0.0) dll_bw_hz = static_cast<float>(FLAGS_dll_bw_hz);
early_late_space_chips = configuration->property(role + ".early_late_space_chips", 0.5);
std::string default_dump_filename = "./track_ch";
dump_filename = configuration->property(role + ".dump_filename", default_dump_filename);
vector_length = std::round(fs_in / (GPS_L1_CA_CODE_RATE_HZ / GPS_L1_CA_CODE_LENGTH_CHIPS));
bce_run = configuration->property(role + ".bce_run", false);
bce_ptrans = configuration->property(role + ".p_transient", 0);
bce_strans = configuration->property(role + ".s_transient", 0);
bce_nu = configuration->property(role + ".bce_nu", 0);
bce_kappa = configuration->property(role + ".bce_kappa", 0);
//################# MAKE TRACKING GNURadio object ###################
if (item_type.compare("gr_complex") == 0)
{
item_size_ = sizeof(gr_complex);
tracking_ = gps_l1_ca_kf_make_tracking_cc(
order,
f_if,
fs_in,
vector_length,
dump,
dump_filename,
dll_bw_hz,
early_late_space_chips,
bce_run,
bce_ptrans,
bce_strans,
bce_nu,
bce_kappa);
}
else
{
item_size_ = sizeof(gr_complex);
LOG(WARNING) << item_type << " unknown tracking item type.";
}
channel_ = 0;
DLOG(INFO) << "tracking(" << tracking_->unique_id() << ")";
}
GpsL1CaKfTracking::~GpsL1CaKfTracking()
{
}
void GpsL1CaKfTracking::start_tracking()
{
tracking_->start_tracking();
}
/*
* Set tracking channel unique ID
*/
void GpsL1CaKfTracking::set_channel(unsigned int channel)
{
channel_ = channel;
tracking_->set_channel(channel);
}
void GpsL1CaKfTracking::set_gnss_synchro(Gnss_Synchro* p_gnss_synchro)
{
tracking_->set_gnss_synchro(p_gnss_synchro);
}
void GpsL1CaKfTracking::connect(gr::top_block_sptr top_block)
{
if (top_block)
{ /* top_block is not null */
};
//nothing to connect, now the tracking uses gr_sync_decimator
}
void GpsL1CaKfTracking::disconnect(gr::top_block_sptr top_block)
{
if (top_block)
{ /* top_block is not null */
};
//nothing to disconnect, now the tracking uses gr_sync_decimator
}
gr::basic_block_sptr GpsL1CaKfTracking::get_left_block()
{
return tracking_;
}
gr::basic_block_sptr GpsL1CaKfTracking::get_right_block()
{
return tracking_;
}

105
src/algorithms/tracking/adapters/gps_l1_ca_kf_tracking.h Normal file
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@ -0,0 +1,105 @@
/*!
* \file GPS_L1_CA_KF_Tracking.h
* \brief Interface of an adapter of a DLL + Kalman carrier
* tracking loop block for GPS L1 C/A signals
* \author Javier Arribas, 2018. jarribas(at)cttc.es
* \author Jordi Vila-Valls 2018. jvila(at)cttc.es
* \author Carles Fernandez-Prades 2018. cfernandez(at)cttc.es
*
* Reference:
* J. Vila-Valls, P. Closas, M. Navarro and C. Fernandez-Prades,
* "Are PLLs Dead? A Tutorial on Kalman Filter-based Techniques for Digital
* Carrier Synchronization", IEEE Aerospace and Electronic Systems Magazine,
* Vol. 32, No. 7, pp. 28–45, July 2017. DOI: 10.1109/MAES.2017.150260
*
* -------------------------------------------------------------------------
*
* Copyright (C) 2010-2018 (see AUTHORS file for a list of contributors)
*
* GNSS-SDR is a software defined Global Navigation
* Satellite Systems receiver
*
* This file is part of GNSS-SDR.
*
* GNSS-SDR is free software: you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation, either version 3 of the License, or
* (at your option) any later version.
*
* GNSS-SDR is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with GNSS-SDR. If not, see <http://www.gnu.org/licenses/>.
*
* -------------------------------------------------------------------------
*/
#ifndef GNSS_SDR_GPS_L1_CA_KF_TRACKING_H_
#define GNSS_SDR_GPS_L1_CA_KF_TRACKING_H_
#include "gps_l1_ca_kf_tracking_cc.h"
#include "tracking_interface.h"
#include <string>
class ConfigurationInterface;
/*!
* \brief This class implements a code DLL + carrier PLL tracking loop
*/
class GpsL1CaKfTracking : public TrackingInterface
{
public:
GpsL1CaKfTracking(ConfigurationInterface* configuration,
std::string role,
unsigned int in_streams,
unsigned int out_streams);
virtual ~GpsL1CaKfTracking();
inline std::string role() override
{
return role_;
}
//! Returns "GPS_L1_CA_KF_Tracking"
inline std::string implementation() override
{
return "GPS_L1_CA_KF_Tracking";
}
inline size_t item_size() override
{
return item_size_;
}
void connect(gr::top_block_sptr top_block) override;
void disconnect(gr::top_block_sptr top_block) override;
gr::basic_block_sptr get_left_block() override;
gr::basic_block_sptr get_right_block() override;
/*!
* \brief Set tracking channel unique ID
*/
void set_channel(unsigned int channel) override;
/*!
* \brief Set acquisition/tracking common Gnss_Synchro object pointer
* to efficiently exchange synchronization data between acquisition and tracking blocks
*/
void set_gnss_synchro(Gnss_Synchro* p_gnss_synchro) override;
void start_tracking() override;
private:
gps_l1_ca_kf_tracking_cc_sptr tracking_;
size_t item_size_;
unsigned int channel_;
std::string role_;
unsigned int in_streams_;
unsigned int out_streams_;
};
#endif // GNSS_SDR_GPS_L1_CA_KF_TRACKING_H_

2
src/algorithms/tracking/gnuradio_blocks/CMakeLists.txt
View File

@ -34,6 +34,7 @@ set(TRACKING_GR_BLOCKS_SOURCES
glonass_l1_ca_dll_pll_tracking_cc.cc
glonass_l1_ca_dll_pll_c_aid_tracking_cc.cc
glonass_l1_ca_dll_pll_c_aid_tracking_sc.cc
gps_l1_ca_kf_tracking_cc.cc
glonass_l2_ca_dll_pll_tracking_cc.cc
glonass_l2_ca_dll_pll_c_aid_tracking_cc.cc
glonass_l2_ca_dll_pll_c_aid_tracking_sc.cc
@ -48,6 +49,7 @@ include_directories(
${CMAKE_SOURCE_DIR}/src/core/receiver
${CMAKE_SOURCE_DIR}/src/algorithms/tracking/libs
${CMAKE_SOURCE_DIR}/src/algorithms/libs
${ARMADILLO_INCLUDE_DIRS}
${GLOG_INCLUDE_DIRS}
${GFlags_INCLUDE_DIRS}
${Boost_INCLUDE_DIRS}

956
src/algorithms/tracking/gnuradio_blocks/gps_l1_ca_kf_tracking_cc.cc Normal file
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@ -0,0 +1,956 @@
/*!
* \file gps_l1_ca_kf_tracking_cc.cc
* \brief Implementation of a processing block of a DLL + Kalman carrier
* tracking loop for GPS L1 C/A signals
* \author Javier Arribas, 2018. jarribas(at)cttc.es
* \author Jordi Vila-Valls 2018. jvila(at)cttc.es
* \author Carles Fernandez-Prades 2018. cfernandez(at)cttc.es
*
* Reference:
* J. Vila-Valls, P. Closas, M. Navarro and C. Fernandez-Prades,
* "Are PLLs Dead? A Tutorial on Kalman Filter-based Techniques for Digital
* Carrier Synchronization", IEEE Aerospace and Electronic Systems Magazine,
* Vol. 32, No. 7, pp. 28–45, July 2017. DOI: 10.1109/MAES.2017.150260
*
* -------------------------------------------------------------------------
*
* Copyright (C) 2010-2018 (see AUTHORS file for a list of contributors)
*
* GNSS-SDR is a software defined Global Navigation
* Satellite Systems receiver
*
* This file is part of GNSS-SDR.
*
* GNSS-SDR is free software: you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation, either version 3 of the License, or
* (at your option) any later version.
*
* GNSS-SDR is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with GNSS-SDR. If not, see <http://www.gnu.org/licenses/>.
*
* -------------------------------------------------------------------------
*/
#include "gps_l1_ca_kf_tracking_cc.h"
#include "gps_sdr_signal_processing.h"
#include "tracking_discriminators.h"
#include "lock_detectors.h"
#include "gnss_sdr_flags.h"
#include "GPS_L1_CA.h"
#include "control_message_factory.h"
#include <boost/lexical_cast.hpp>
#include <gnuradio/io_signature.h>
#include <glog/logging.h>
#include <volk_gnsssdr/volk_gnsssdr.h>
#include <matio.h>
#include <cmath>
#include <iostream>
#include <memory>
#include <sstream>
using google::LogMessage;
gps_l1_ca_kf_tracking_cc_sptr
gps_l1_ca_kf_make_tracking_cc(
uint32_t order,
int64_t if_freq,
int64_t fs_in,
uint32_t vector_length,
bool dump,
std::string dump_filename,
float dll_bw_hz,
float early_late_space_chips,
bool bce_run,
uint32_t bce_ptrans,
uint32_t bce_strans,
int32_t bce_nu,
int32_t bce_kappa)
{
return gps_l1_ca_kf_tracking_cc_sptr(new Gps_L1_Ca_Kf_Tracking_cc(order, if_freq,
fs_in, vector_length, dump, dump_filename, dll_bw_hz, early_late_space_chips,
bce_run, bce_ptrans, bce_strans, bce_nu, bce_kappa));
}
void Gps_L1_Ca_Kf_Tracking_cc::forecast(int noutput_items,
gr_vector_int &ninput_items_required)
{
if (noutput_items != 0)
{
ninput_items_required[0] = static_cast<int>(d_vector_length) * 2; // set the required available samples in each call
}
}
Gps_L1_Ca_Kf_Tracking_cc::Gps_L1_Ca_Kf_Tracking_cc(
uint32_t order,
int64_t if_freq,
int64_t fs_in,
uint32_t vector_length,
bool dump,
std::string dump_filename,
float dll_bw_hz,
float early_late_space_chips,
bool bce_run,
uint32_t bce_ptrans,
uint32_t bce_strans,
int32_t bce_nu,
int32_t bce_kappa) : gr::block("Gps_L1_Ca_Kf_Tracking_cc", gr::io_signature::make(1, 1, sizeof(gr_complex)),
gr::io_signature::make(1, 1, sizeof(Gnss_Synchro)))
{
// Telemetry bit synchronization message port input
this->message_port_register_in(pmt::mp("preamble_timestamp_s"));
this->message_port_register_out(pmt::mp("events"));
// initialize internal vars
d_order = order;
d_dump = dump;
d_if_freq = if_freq;
d_fs_in = fs_in;
d_vector_length = vector_length;
d_dump_filename = dump_filename;
d_current_prn_length_samples = static_cast<int>(d_vector_length);
// Initialize tracking ==========================================
d_code_loop_filter.set_DLL_BW(dll_bw_hz);
// --- DLL variables --------------------------------------------------------
d_early_late_spc_chips = early_late_space_chips; // Define early-late offset (in chips)
// Initialization of local code replica
// Get space for a vector with the C/A code replica sampled 1x/chip
d_ca_code = static_cast<float *>(volk_gnsssdr_malloc(static_cast<int>(GPS_L1_CA_CODE_LENGTH_CHIPS) * sizeof(float), volk_gnsssdr_get_alignment()));
// correlator outputs (scalar)
d_n_correlator_taps = 3; // Early, Prompt, and Late
d_correlator_outs = static_cast<gr_complex *>(volk_gnsssdr_malloc(d_n_correlator_taps * sizeof(gr_complex), volk_gnsssdr_get_alignment()));
for (int32_t n = 0; n < d_n_correlator_taps; n++)
{
d_correlator_outs[n] = gr_complex(0, 0);
}
d_local_code_shift_chips = static_cast<float *>(volk_gnsssdr_malloc(d_n_correlator_taps * sizeof(float), volk_gnsssdr_get_alignment()));
// Set TAPs delay values [chips]
d_local_code_shift_chips[0] = -d_early_late_spc_chips;
d_local_code_shift_chips[1] = 0.0;
d_local_code_shift_chips[2] = d_early_late_spc_chips;
multicorrelator_cpu.init(2 * d_current_prn_length_samples, d_n_correlator_taps);
// --- Perform initializations ------------------------------
// define initial code frequency basis of NCO
d_code_freq_chips = GPS_L1_CA_CODE_RATE_HZ;
// define residual code phase (in chips)
d_rem_code_phase_samples = 0.0;
// define residual carrier phase
d_rem_carr_phase_rad = 0.0;
// define residual carrier phase covariance
d_carr_phase_sigma2 = 0.0;
// sample synchronization
d_sample_counter = 0;
d_acq_sample_stamp = 0;
d_enable_tracking = false;
d_pull_in = false;
// CN0 estimation and lock detector buffers
d_cn0_estimation_counter = 0;
d_Prompt_buffer = new gr_complex[FLAGS_cn0_samples];
d_carrier_lock_test = 1;
d_CN0_SNV_dB_Hz = 0;
d_carrier_lock_fail_counter = 0;
d_carrier_lock_threshold = FLAGS_carrier_lock_th;
systemName["G"] = std::string("GPS");
systemName["S"] = std::string("SBAS");
d_acquisition_gnss_synchro = 0;
d_channel = 0;
d_acq_code_phase_samples = 0.0;
d_acq_carrier_doppler_hz = 0.0;
d_carrier_doppler_hz = 0.0;
d_carrier_dopplerrate_hz2 = 0.0;
d_acc_carrier_phase_rad = 0.0;
d_code_phase_samples = 0.0;
d_rem_code_phase_chips = 0.0;
d_code_phase_step_chips = 0.0;
d_carrier_phase_step_rad = 0.0;
code_error_chips = 0.0;
code_error_filt_chips = 0.0;
set_relative_rate(1.0 / static_cast<double>(d_vector_length));
// Kalman filter initialization (receiver initialization)
double CN_dB_Hz = 30;
double CN_lin = pow(10, CN_dB_Hz / 10.0);
double sigma2_phase_detector_cycles2;
sigma2_phase_detector_cycles2 = (1.0 / (2.0 * CN_lin * GPS_L1_CA_CODE_PERIOD)) * (1.0 + 1.0 / (2.0 * CN_lin * GPS_L1_CA_CODE_PERIOD));
// covariances (static)
double sigma2_carrier_phase = GPS_TWO_PI / 4;
double sigma2_doppler = 450;
double sigma2_doppler_rate = pow(4.0 * GPS_TWO_PI, 2) / 12.0;
kf_P_x_ini = arma::zeros(2, 2);
kf_P_x_ini(0, 0) = sigma2_carrier_phase;
kf_P_x_ini(1, 1) = sigma2_doppler;
kf_R = arma::zeros(1, 1);
kf_R(0, 0) = sigma2_phase_detector_cycles2;
kf_Q = arma::zeros(2, 2);
kf_Q(0, 0) = pow(GPS_L1_CA_CODE_PERIOD, 4);
kf_Q(1, 1) = GPS_L1_CA_CODE_PERIOD;
kf_F = arma::zeros(2, 2);
kf_F(0, 0) = 1.0;
kf_F(0, 1) = GPS_TWO_PI * GPS_L1_CA_CODE_PERIOD;
kf_F(1, 0) = 0.0;
kf_F(1, 1) = 1.0;
kf_H = arma::zeros(1, 2);
kf_H(0, 0) = 1.0;
kf_x = arma::zeros(2, 1);
kf_y = arma::zeros(1, 1);
kf_P_y = arma::zeros(1, 1);
// order three
if (d_order == 3)
{
kf_P_x_ini = arma::resize(kf_P_x_ini, 3, 3);
kf_P_x_ini(2, 2) = sigma2_doppler_rate;
kf_Q = arma::zeros(3, 3);
kf_Q(0, 0) = pow(GPS_L1_CA_CODE_PERIOD, 4);
kf_Q(1, 1) = GPS_L1_CA_CODE_PERIOD;
kf_Q(2, 2) = GPS_L1_CA_CODE_PERIOD;
kf_F = arma::resize(kf_F, 3, 3);
kf_F(0, 2) = 0.5 * GPS_TWO_PI * pow(GPS_L1_CA_CODE_PERIOD, 2);
kf_F(1, 2) = GPS_L1_CA_CODE_PERIOD;
kf_F(2, 0) = 0.0;
kf_F(2, 1) = 0.0;
kf_F(2, 2) = 1.0;
kf_H = arma::resize(kf_H, 1, 3);
kf_H(0, 2) = 0.0;
kf_x = arma::resize(kf_x, 3, 1);
kf_x(2, 0) = 0.0;
}
// Bayesian covariance estimator initialization
kf_iter = 0;
bayes_run = bce_run;
bayes_ptrans = bce_ptrans;
bayes_strans = bce_strans;
bayes_kappa = bce_kappa;
bayes_nu = bce_nu;
kf_R_est = kf_R;
bayes_estimator.init(arma::zeros(1, 1), bayes_kappa, bayes_nu, (kf_H * kf_P_x_ini * kf_H.t() + kf_R) * (bayes_nu + 2));
}
void Gps_L1_Ca_Kf_Tracking_cc::start_tracking()
{
/*
* correct the code phase according to the delay between acq and trk
*/
d_acq_code_phase_samples = d_acquisition_gnss_synchro->Acq_delay_samples;
d_acq_carrier_doppler_hz = d_acquisition_gnss_synchro->Acq_doppler_hz;
d_acq_sample_stamp = d_acquisition_gnss_synchro->Acq_samplestamp_samples;
d_acq_carrier_doppler_step_hz = static_cast<double>(d_acquisition_gnss_synchro->Acq_doppler_step);
// Correct Kalman filter covariance according to acq doppler step size (3 sigma)
if (d_acquisition_gnss_synchro->Acq_doppler_step > 0)
{
kf_P_x_ini(1, 1) = pow(d_acq_carrier_doppler_step_hz / 3.0, 2);
bayes_estimator.init(arma::zeros(1, 1), bayes_kappa, bayes_nu, (kf_H * kf_P_x_ini * kf_H.t() + kf_R) * (bayes_nu + 2));
}
int64_t acq_trk_diff_samples;
double acq_trk_diff_seconds;
acq_trk_diff_samples = static_cast<int64_t>(d_sample_counter) - static_cast<int64_t>(d_acq_sample_stamp); //-d_vector_length;
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);
// Doppler effect Fd = (C / (C + Vr)) * F
double radial_velocity = (GPS_L1_FREQ_HZ + d_acq_carrier_doppler_hz) / GPS_L1_FREQ_HZ;
// new chip and prn sequence periods based on acq Doppler
double T_chip_mod_seconds;
double T_prn_mod_seconds;
double T_prn_mod_samples;
d_code_freq_chips = radial_velocity * GPS_L1_CA_CODE_RATE_HZ;
d_code_phase_step_chips = static_cast<double>(d_code_freq_chips) / static_cast<double>(d_fs_in);
T_chip_mod_seconds = 1 / d_code_freq_chips;
T_prn_mod_seconds = T_chip_mod_seconds * GPS_L1_CA_CODE_LENGTH_CHIPS;
T_prn_mod_samples = T_prn_mod_seconds * static_cast<double>(d_fs_in);
d_current_prn_length_samples = round(T_prn_mod_samples);
double T_prn_true_seconds = GPS_L1_CA_CODE_LENGTH_CHIPS / GPS_L1_CA_CODE_RATE_HZ;
double T_prn_true_samples = T_prn_true_seconds * static_cast<double>(d_fs_in);
double T_prn_diff_seconds = T_prn_true_seconds - T_prn_mod_seconds;
double N_prn_diff = acq_trk_diff_seconds / T_prn_true_seconds;
double corrected_acq_phase_samples, delay_correction_samples;
corrected_acq_phase_samples = fmod((d_acq_code_phase_samples + T_prn_diff_seconds * N_prn_diff * static_cast<double>(d_fs_in)), T_prn_true_samples);
if (corrected_acq_phase_samples < 0)
{
corrected_acq_phase_samples = T_prn_mod_samples + corrected_acq_phase_samples;
}
delay_correction_samples = d_acq_code_phase_samples - corrected_acq_phase_samples;
d_acq_code_phase_samples = corrected_acq_phase_samples;
d_carrier_doppler_hz = d_acq_carrier_doppler_hz;
d_carrier_dopplerrate_hz2 = 0;
d_carrier_phase_step_rad = GPS_TWO_PI * d_carrier_doppler_hz / static_cast<double>(d_fs_in);
// DLL filter initialization
d_code_loop_filter.initialize(); // initialize the code filter
// generate local reference ALWAYS starting at chip 1 (1 sample per chip)
gps_l1_ca_code_gen_float(d_ca_code, d_acquisition_gnss_synchro->PRN, 0);
multicorrelator_cpu.set_local_code_and_taps(static_cast<int>(GPS_L1_CA_CODE_LENGTH_CHIPS), d_ca_code, d_local_code_shift_chips);
for (int32_t n = 0; n < d_n_correlator_taps; n++)
{
d_correlator_outs[n] = gr_complex(0, 0);
}
d_carrier_lock_fail_counter = 0;
d_rem_code_phase_samples = 0;
d_rem_carr_phase_rad = 0.0;
d_rem_code_phase_chips = 0.0;
d_acc_carrier_phase_rad = 0.0;
d_carr_phase_sigma2 = 0.0;
d_code_phase_samples = d_acq_code_phase_samples;
std::string sys_ = &d_acquisition_gnss_synchro->System;
sys = sys_.substr(0, 1);
// DEBUG OUTPUT
std::cout << "Tracking of GPS L1 C/A signal started on channel " << d_channel << " for satellite " << Gnss_Satellite(systemName[sys], d_acquisition_gnss_synchro->PRN) << std::endl;
LOG(INFO) << "Starting tracking of satellite " << Gnss_Satellite(systemName[sys], d_acquisition_gnss_synchro->PRN) << " on channel " << d_channel;
// enable tracking
d_pull_in = true;
d_enable_tracking = true;
LOG(INFO) << "PULL-IN Doppler [Hz]=" << d_carrier_doppler_hz
<< " Code Phase correction [samples]=" << delay_correction_samples
<< " PULL-IN Code Phase [samples]=" << d_acq_code_phase_samples;
}
Gps_L1_Ca_Kf_Tracking_cc::~Gps_L1_Ca_Kf_Tracking_cc()
{
if (d_dump_file.is_open())
{
try
{
d_dump_file.close();
}
catch (const std::exception &ex)
{
LOG(WARNING) << "Exception in destructor " << ex.what();
}
}
if (d_dump)
{
if (d_channel == 0)
{
std::cout << "Writing .mat files ...";
}
Gps_L1_Ca_Kf_Tracking_cc::save_matfile();
if (d_channel == 0)
{
std::cout << " done." << std::endl;
}
}
try
{
volk_gnsssdr_free(d_local_code_shift_chips);
volk_gnsssdr_free(d_correlator_outs);
volk_gnsssdr_free(d_ca_code);
delete[] d_Prompt_buffer;
multicorrelator_cpu.free();
}
catch (const std::exception &ex)
{
LOG(WARNING) << "Exception in destructor " << ex.what();
}
}
int32_t Gps_L1_Ca_Kf_Tracking_cc::save_matfile()
{
// READ DUMP FILE
std::ifstream::pos_type size;
int32_t number_of_double_vars = 1;
int32_t number_of_float_vars = 19;
int32_t epoch_size_bytes = sizeof(uint64_t) + sizeof(double) * number_of_double_vars +
sizeof(float) * number_of_float_vars + sizeof(uint32_t);
std::ifstream dump_file;
dump_file.exceptions(std::ifstream::failbit | std::ifstream::badbit);
try
{
dump_file.open(d_dump_filename.c_str(), std::ios::binary | std::ios::ate);
}
catch (const std::ifstream::failure &e)
{
std::cerr << "Problem opening dump file:" << e.what() << std::endl;
return 1;
}
// count number of epochs and rewind
int64_t num_epoch = 0;
if (dump_file.is_open())
{
size = dump_file.tellg();
num_epoch = static_cast<int64_t>(size) / static_cast<int64_t>(epoch_size_bytes);
dump_file.seekg(0, std::ios::beg);
}
else
{
return 1;
}
float *abs_VE = new float[num_epoch];
float *abs_E = new float[num_epoch];
float *abs_P = new float[num_epoch];
float *abs_L = new float[num_epoch];
float *abs_VL = new float[num_epoch];
float *Prompt_I = new float[num_epoch];
float *Prompt_Q = new float[num_epoch];
uint64_t *PRN_start_sample_count = new uint64_t[num_epoch];
float *acc_carrier_phase_rad = new float[num_epoch];
float *carrier_doppler_hz = new float[num_epoch];
float *carrier_dopplerrate_hz2 = new float[num_epoch];
float *code_freq_chips = new float[num_epoch];
float *carr_error_hz = new float[num_epoch];
float *carr_noise_sigma2 = new float[num_epoch];
float *carr_error_filt_hz = new float[num_epoch];
float *code_error_chips = new float[num_epoch];
float *code_error_filt_chips = new float[num_epoch];
float *CN0_SNV_dB_Hz = new float[num_epoch];
float *carrier_lock_test = new float[num_epoch];
float *aux1 = new float[num_epoch];
double *aux2 = new double[num_epoch];
uint32_t *PRN = new uint32_t[num_epoch];
try
{
if (dump_file.is_open())
{
for (int64_t i = 0; i < num_epoch; i++)
{
dump_file.read(reinterpret_cast<char *>(&abs_VE[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&abs_E[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&abs_P[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&abs_L[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&abs_VL[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&Prompt_I[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&Prompt_Q[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&PRN_start_sample_count[i]), sizeof(uint64_t));
dump_file.read(reinterpret_cast<char *>(&acc_carrier_phase_rad[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&carrier_doppler_hz[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&carrier_dopplerrate_hz2[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&code_freq_chips[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&carr_error_hz[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&carr_noise_sigma2[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&carr_error_filt_hz[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&code_error_chips[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&code_error_filt_chips[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&CN0_SNV_dB_Hz[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&carrier_lock_test[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&aux1[i]), sizeof(float));
dump_file.read(reinterpret_cast<char *>(&aux2[i]), sizeof(double));
dump_file.read(reinterpret_cast<char *>(&PRN[i]), sizeof(uint32_t));
}
}
dump_file.close();
}
catch (const std::ifstream::failure &e)
{
std::cerr << "Problem reading dump file:" << e.what() << std::endl;
delete[] abs_VE;
delete[] abs_E;
delete[] abs_P;
delete[] abs_L;
delete[] abs_VL;
delete[] Prompt_I;
delete[] Prompt_Q;
delete[] PRN_start_sample_count;
delete[] acc_carrier_phase_rad;
delete[] carrier_doppler_hz;
delete[] carrier_dopplerrate_hz2;
delete[] code_freq_chips;
delete[] carr_error_hz;
delete[] carr_noise_sigma2;
delete[] carr_error_filt_hz;
delete[] code_error_chips;
delete[] code_error_filt_chips;
delete[] CN0_SNV_dB_Hz;
delete[] carrier_lock_test;
delete[] aux1;
delete[] aux2;
delete[] PRN;
return 1;
}
// WRITE MAT FILE
mat_t *matfp;
matvar_t *matvar;
std::string filename = d_dump_filename;
filename.erase(filename.length() - 4, 4);
filename.append(".mat");
matfp = Mat_CreateVer(filename.c_str(), NULL, MAT_FT_MAT73);
if (reinterpret_cast<long *>(matfp) != NULL)
{
size_t dims[2] = {1, static_cast<size_t>(num_epoch)};
matvar = Mat_VarCreate("abs_VE", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, abs_VE, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("abs_E", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, abs_E, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("abs_P", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, abs_P, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("abs_L", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, abs_L, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("abs_VL", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, abs_VL, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("Prompt_I", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, Prompt_I, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("Prompt_Q", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, Prompt_Q, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("PRN_start_sample_count", MAT_C_UINT64, MAT_T_UINT64, 2, dims, PRN_start_sample_count, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("acc_carrier_phase_rad", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, acc_carrier_phase_rad, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("carrier_doppler_hz", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, carrier_doppler_hz, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("carrier_dopplerrate_hz2", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, carrier_dopplerrate_hz2, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("code_freq_chips", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, code_freq_chips, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("carr_error_hz", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, carr_error_hz, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("carr_noise_sigma2", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, carr_noise_sigma2, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("carr_error_filt_hz", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, carr_error_filt_hz, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("code_error_chips", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, code_error_chips, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("code_error_filt_chips", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, code_error_filt_chips, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("CN0_SNV_dB_Hz", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, CN0_SNV_dB_Hz, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("carrier_lock_test", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, carrier_lock_test, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("aux1", MAT_C_SINGLE, MAT_T_SINGLE, 2, dims, aux1, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("aux2", MAT_C_DOUBLE, MAT_T_DOUBLE, 2, dims, aux2, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
matvar = Mat_VarCreate("PRN", MAT_C_UINT32, MAT_T_UINT32, 2, dims, PRN, 0);
Mat_VarWrite(matfp, matvar, MAT_COMPRESSION_ZLIB); // or MAT_COMPRESSION_NONE
Mat_VarFree(matvar);
}
Mat_Close(matfp);
delete[] abs_VE;
delete[] abs_E;
delete[] abs_P;
delete[] abs_L;
delete[] abs_VL;
delete[] Prompt_I;
delete[] Prompt_Q;
delete[] PRN_start_sample_count;
delete[] acc_carrier_phase_rad;
delete[] carrier_doppler_hz;
delete[] carrier_dopplerrate_hz2;
delete[] code_freq_chips;
delete[] carr_error_hz;
delete[] carr_noise_sigma2;
delete[] carr_error_filt_hz;
delete[] code_error_chips;
delete[] code_error_filt_chips;
delete[] CN0_SNV_dB_Hz;
delete[] carrier_lock_test;
delete[] aux1;
delete[] aux2;
delete[] PRN;
return 0;
}
void Gps_L1_Ca_Kf_Tracking_cc::set_channel(uint32_t channel)
{
gr::thread::scoped_lock l(d_setlock);
d_channel = channel;
LOG(INFO) << "Tracking Channel set to " << d_channel;
// ############# ENABLE DATA FILE LOG #################
if (d_dump)
{
if (!d_dump_file.is_open())
{
try
{
d_dump_filename.append(boost::lexical_cast<std::string>(d_channel));
d_dump_filename.append(".dat");
d_dump_file.exceptions(std::ifstream::failbit | std::ifstream::badbit);
d_dump_file.open(d_dump_filename.c_str(), std::ios::out | std::ios::binary);
LOG(INFO) << "Tracking dump enabled on channel " << d_channel << " Log file: " << d_dump_filename.c_str();
}
catch (const std::ifstream::failure &e)
{
LOG(WARNING) << "channel " << d_channel << " Exception opening trk dump file " << e.what();
}
}
}
}
void Gps_L1_Ca_Kf_Tracking_cc::set_gnss_synchro(Gnss_Synchro *p_gnss_synchro)
{
d_acquisition_gnss_synchro = p_gnss_synchro;
}
int Gps_L1_Ca_Kf_Tracking_cc::general_work(int noutput_items __attribute__((unused)), gr_vector_int &ninput_items __attribute__((unused)),
gr_vector_const_void_star &input_items, gr_vector_void_star &output_items)
{
// process vars
d_carr_phase_error_rad = 0.0;
double code_error_chips = 0.0;
double code_error_filt_chips = 0.0;
// Block input data and block output stream pointers
const gr_complex *in = reinterpret_cast<const gr_complex *>(input_items[0]);
Gnss_Synchro **out = reinterpret_cast<Gnss_Synchro **>(&output_items[0]);
// GNSS_SYNCHRO OBJECT to interchange data between tracking->telemetry_decoder
Gnss_Synchro current_synchro_data = Gnss_Synchro();
if (d_enable_tracking == true)
{
// Fill the acquisition data
current_synchro_data = *d_acquisition_gnss_synchro;
// Receiver signal alignment
if (d_pull_in == true)
{
// Signal alignment (skip samples until the incoming signal is aligned with local replica)
uint64_t acq_to_trk_delay_samples = d_sample_counter - d_acq_sample_stamp;
double acq_trk_shif_correction_samples = static_cast<double>(d_current_prn_length_samples) - std::fmod(static_cast<double>(acq_to_trk_delay_samples), static_cast<double>(d_current_prn_length_samples));
int32_t samples_offset = std::round(d_acq_code_phase_samples + acq_trk_shif_correction_samples);
if (samples_offset < 0)
{
samples_offset = 0;
}
d_acc_carrier_phase_rad -= d_carrier_phase_step_rad * d_acq_code_phase_samples;
d_sample_counter += samples_offset; // count for the processed samples
d_pull_in = false;
current_synchro_data.Carrier_phase_rads = d_acc_carrier_phase_rad;
current_synchro_data.Carrier_Doppler_hz = d_carrier_doppler_hz;
current_synchro_data.fs = d_fs_in;
current_synchro_data.correlation_length_ms = 1;
*out[0] = current_synchro_data;
// Kalman filter initialization reset
kf_P_x = kf_P_x_ini;
// Update Kalman states based on acquisition information
kf_x(0) = d_carrier_phase_step_rad * samples_offset;
kf_x(1) = d_carrier_doppler_hz;
if (kf_x.n_elem > 2)
{
kf_x(2) = d_carrier_dopplerrate_hz2;
}
// Covariance estimation initialization reset
kf_iter = 0;
bayes_estimator.init(arma::zeros(1, 1), bayes_kappa, bayes_nu, (kf_H * kf_P_x_ini * kf_H.t() + kf_R) * (bayes_nu + 2));
consume_each(samples_offset); // shift input to perform alignment with local replica
return 1;
}
// ################# CARRIER WIPEOFF AND CORRELATORS ##############################
// Perform carrier wipe-off and compute Early, Prompt and Late correlation
multicorrelator_cpu.set_input_output_vectors(d_correlator_outs, in);
multicorrelator_cpu.Carrier_wipeoff_multicorrelator_resampler(d_rem_carr_phase_rad,
d_carrier_phase_step_rad,
d_rem_code_phase_chips,
d_code_phase_step_chips,
d_current_prn_length_samples);
// ################## Kalman Carrier Tracking ######################################
// Kalman state prediction (time update)
kf_x_pre = kf_F * kf_x; //state prediction
kf_P_x_pre = kf_F * kf_P_x * kf_F.t() + kf_Q; //state error covariance prediction
// Update discriminator [rads/Ti]
d_carr_phase_error_rad = pll_cloop_two_quadrant_atan(d_correlator_outs[1]); // prompt output
// Kalman estimation (measurement update)
double sigma2_phase_detector_cycles2;
double CN_lin = pow(10, d_CN0_SNV_dB_Hz / 10.0);
sigma2_phase_detector_cycles2 = (1.0 / (2.0 * CN_lin * GPS_L1_CA_CODE_PERIOD)) * (1.0 + 1.0 / (2.0 * CN_lin * GPS_L1_CA_CODE_PERIOD));
kf_y(0) = d_carr_phase_error_rad; // measurement vector
kf_R(0, 0) = sigma2_phase_detector_cycles2;
if (bayes_run && (kf_iter >= bayes_ptrans))
{
bayes_estimator.update_sequential(kf_y);
}
if (bayes_run && (kf_iter >= (bayes_ptrans + bayes_strans)))
{
// TODO: Resolve segmentation fault
kf_P_y = bayes_estimator.get_Psi_est();
kf_R_est = kf_P_y - kf_H * kf_P_x_pre * kf_H.t();
}
else
{
kf_P_y = kf_H * kf_P_x_pre * kf_H.t() + kf_R; // innovation covariance matrix
kf_R_est = kf_R;
}
// Kalman filter update step
kf_K = (kf_P_x_pre * kf_H.t()) * arma::inv(kf_P_y); // Kalman gain
kf_x = kf_x_pre + kf_K * kf_y; // updated state estimation
kf_P_x = (arma::eye(size(kf_P_x_pre)) - kf_K * kf_H) * kf_P_x_pre; // update state estimation error covariance matrix
// Store Kalman filter results
d_rem_carr_phase_rad = kf_x(0); // set a new carrier Phase estimation to the NCO
d_carrier_doppler_hz = kf_x(1); // set a new carrier Doppler estimation to the NCO
if (kf_x.n_elem > 2)
{
d_carrier_dopplerrate_hz2 = kf_x(2);
}
else
{
d_carrier_dopplerrate_hz2 = 0;
}
d_carr_phase_sigma2 = kf_R_est(0, 0);
// ################## DLL ##########################################################
// New code Doppler frequency estimation based on carrier frequency estimation
d_code_freq_chips = GPS_L1_CA_CODE_RATE_HZ + ((d_carrier_doppler_hz * GPS_L1_CA_CODE_RATE_HZ) / GPS_L1_FREQ_HZ);
// DLL discriminator
code_error_chips = dll_nc_e_minus_l_normalized(d_correlator_outs[0], d_correlator_outs[2]); // [chips/Ti] early and late
// Code discriminator filter
code_error_filt_chips = d_code_loop_filter.get_code_nco(code_error_chips); // [chips/second]
double T_chip_seconds = 1.0 / static_cast<double>(d_code_freq_chips);
double T_prn_seconds = T_chip_seconds * GPS_L1_CA_CODE_LENGTH_CHIPS;
double code_error_filt_secs = (T_prn_seconds * code_error_filt_chips * T_chip_seconds); // [seconds]
// ################## CARRIER AND CODE NCO BUFFER ALIGNMENT #######################
// keep alignment parameters for the next input buffer
// Compute the next buffer length based in the new period of the PRN sequence and the code phase error estimation
double T_prn_samples = T_prn_seconds * static_cast<double>(d_fs_in);
double K_blk_samples = T_prn_samples + d_rem_code_phase_samples + code_error_filt_secs * static_cast<double>(d_fs_in);
d_current_prn_length_samples = static_cast<int>(round(K_blk_samples)); // round to a discrete number of samples
//################### NCO COMMANDS #################################################
// carrier phase step (NCO phase increment per sample) [rads/sample]
d_carrier_phase_step_rad = PI_2 * d_carrier_doppler_hz / static_cast<double>(d_fs_in);
// carrier phase accumulator
d_acc_carrier_phase_rad -= d_carrier_phase_step_rad * static_cast<double>(d_current_prn_length_samples);
//################### DLL COMMANDS #################################################
// code phase step (Code resampler phase increment per sample) [chips/sample]
d_code_phase_step_chips = d_code_freq_chips / static_cast<double>(d_fs_in);
// remnant code phase [chips]
d_rem_code_phase_samples = K_blk_samples - static_cast<double>(d_current_prn_length_samples); // rounding error < 1 sample
d_rem_code_phase_chips = d_code_freq_chips * (d_rem_code_phase_samples / static_cast<double>(d_fs_in));
// ####### CN0 ESTIMATION AND LOCK DETECTORS ######
if (d_cn0_estimation_counter < FLAGS_cn0_samples)
{
// fill buffer with prompt correlator output values
d_Prompt_buffer[d_cn0_estimation_counter] = d_correlator_outs[1]; //prompt
d_cn0_estimation_counter++;
}
else
{
d_cn0_estimation_counter = 0;
// Code lock indicator
d_CN0_SNV_dB_Hz = cn0_svn_estimator(d_Prompt_buffer, FLAGS_cn0_samples, GPS_L1_CA_CODE_PERIOD);
// Carrier lock indicator
d_carrier_lock_test = carrier_lock_detector(d_Prompt_buffer, FLAGS_cn0_samples);
// Loss of lock detection
if (d_carrier_lock_test < d_carrier_lock_threshold or d_CN0_SNV_dB_Hz < FLAGS_cn0_min)
{
//if (d_channel == 1)
//std::cout << "Carrier Lock Test Fail in channel " << d_channel << ": " << d_carrier_lock_test << " < " << d_carrier_lock_threshold << "," << nfail++ << std::endl;
d_carrier_lock_fail_counter++;
//nfail++;
}
else
{
if (d_carrier_lock_fail_counter > 0) d_carrier_lock_fail_counter--;
}
if (d_carrier_lock_fail_counter > FLAGS_max_lock_fail)
{
std::cout << "Loss of lock in channel " << d_channel << "!" << std::endl;
LOG(INFO) << "Loss of lock in channel " << d_channel << "!";
this->message_port_pub(pmt::mp("events"), pmt::from_long(3)); // 3 -> loss of lock
d_carrier_lock_fail_counter = 0;
d_enable_tracking = false;
}
}
// ########### Output the tracking data to navigation and PVT ##########
current_synchro_data.Prompt_I = static_cast<double>((d_correlator_outs[1]).real());
current_synchro_data.Prompt_Q = static_cast<double>((d_correlator_outs[1]).imag());
current_synchro_data.Tracking_sample_counter = d_sample_counter + static_cast<uint64_t>(d_current_prn_length_samples);
current_synchro_data.Code_phase_samples = d_rem_code_phase_samples;
current_synchro_data.Carrier_phase_rads = d_acc_carrier_phase_rad;
current_synchro_data.Carrier_Doppler_hz = d_carrier_doppler_hz;
current_synchro_data.CN0_dB_hz = d_CN0_SNV_dB_Hz;
current_synchro_data.Flag_valid_symbol_output = true;
current_synchro_data.correlation_length_ms = 1;
kf_iter++;
}
else
{
for (int32_t n = 0; n < d_n_correlator_taps; n++)
{
d_correlator_outs[n] = gr_complex(0, 0);
}
current_synchro_data.Tracking_sample_counter = d_sample_counter + static_cast<uint64_t>(d_current_prn_length_samples);
current_synchro_data.System = {'G'};
current_synchro_data.correlation_length_ms = 1;
}
// assign the GNU Radio block output data
current_synchro_data.fs = d_fs_in;
*out[0] = current_synchro_data;
if (d_dump)
{
// MULTIPLEXED FILE RECORDING - Record results to file
float prompt_I;
float prompt_Q;
float tmp_E, tmp_P, tmp_L;
float tmp_VE = 0.0;
float tmp_VL = 0.0;
float tmp_float;
double tmp_double;
prompt_I = d_correlator_outs[1].real();
prompt_Q = d_correlator_outs[1].imag();
tmp_E = std::abs<float>(d_correlator_outs[0]);
tmp_P = std::abs<float>(d_correlator_outs[1]);
tmp_L = std::abs<float>(d_correlator_outs[2]);
try
{
// EPR
d_dump_file.write(reinterpret_cast<char *>(&tmp_VE), sizeof(float));
d_dump_file.write(reinterpret_cast<char *>(&tmp_E), sizeof(float));
d_dump_file.write(reinterpret_cast<char *>(&tmp_P), sizeof(float));
d_dump_file.write(reinterpret_cast<char *>(&tmp_L), sizeof(float));
d_dump_file.write(reinterpret_cast<char *>(&tmp_VL), sizeof(float));
// PROMPT I and Q (to analyze navigation symbols)
d_dump_file.write(reinterpret_cast<char *>(&prompt_I), sizeof(float));
d_dump_file.write(reinterpret_cast<char *>(&prompt_Q), sizeof(float));
// PRN start sample stamp
d_dump_file.write(reinterpret_cast<char *>(&d_sample_counter), sizeof(uint64_t));
// accumulated carrier phase
tmp_float = d_acc_carrier_phase_rad;
d_dump_file.write(reinterpret_cast<char *>(&tmp_float), sizeof(float));
// carrier and code frequency
tmp_float = d_carrier_doppler_hz;
d_dump_file.write(reinterpret_cast<char *>(&tmp_float), sizeof(float));
tmp_float = d_carrier_dopplerrate_hz2;
d_dump_file.write(reinterpret_cast<char *>(&tmp_float), sizeof(float));
tmp_float = d_code_freq_chips;
d_dump_file.write(reinterpret_cast<char *>(&tmp_float), sizeof(float));
// Kalman commands
tmp_float = static_cast<float>(d_carr_phase_error_rad * GPS_TWO_PI);
d_dump_file.write(reinterpret_cast<char *>(&tmp_float), sizeof(float));
tmp_float = static_cast<float>(d_carr_phase_sigma2);
d_dump_file.write(reinterpret_cast<char *>(&tmp_float), sizeof(float));
tmp_float = static_cast<float>(d_rem_carr_phase_rad * GPS_TWO_PI);
d_dump_file.write(reinterpret_cast<char *>(&tmp_float), sizeof(float));
// DLL commands
tmp_float = code_error_chips;
d_dump_file.write(reinterpret_cast<char *>(&tmp_float), sizeof(float));
tmp_float = code_error_filt_chips;
d_dump_file.write(reinterpret_cast<char *>(&tmp_float), sizeof(float));
// CN0 and carrier lock test
tmp_float = d_CN0_SNV_dB_Hz;
d_dump_file.write(reinterpret_cast<char *>(&tmp_float), sizeof(float));
tmp_float = d_carrier_lock_test;
d_dump_file.write(reinterpret_cast<char *>(&tmp_float), sizeof(float));
// AUX vars (for debug purposes)
tmp_float = d_rem_code_phase_samples;
d_dump_file.write(reinterpret_cast<char *>(&tmp_float), sizeof(float));
tmp_double = static_cast<double>(d_sample_counter + static_cast<uint64_t>(d_current_prn_length_samples));
d_dump_file.write(reinterpret_cast<char *>(&tmp_double), sizeof(double));
// PRN
uint32_t prn_ = d_acquisition_gnss_synchro->PRN;
d_dump_file.write(reinterpret_cast<char *>(&prn_), sizeof(uint32_t));
}
catch (const std::ifstream::failure &e)
{
LOG(WARNING) << "Exception writing trk dump file " << e.what();
}
}
consume_each(d_current_prn_length_samples); // this is necessary in gr::block derivates
d_sample_counter += d_current_prn_length_samples; // count for the processed samples
return 1; // output tracking result ALWAYS even in the case of d_enable_tracking==false
}

221
src/algorithms/tracking/gnuradio_blocks/gps_l1_ca_kf_tracking_cc.h Normal file
View File

@ -0,0 +1,221 @@
/*!
* \file gps_l1_ca_kf_tracking_cc.cc
* \brief Interface of a processing block of a DLL + Kalman carrier
* tracking loop for GPS L1 C/A signals
* \author Javier Arribas, 2018. jarribas(at)cttc.es
* \author Jordi Vila-Valls 2018. jvila(at)cttc.es
* \author Carles Fernandez-Prades 2018. cfernandez(at)cttc.es
*
* Reference:
* J. Vila-Valls, P. Closas, M. Navarro and C. Fernandez-Prades,
* "Are PLLs Dead? A Tutorial on Kalman Filter-based Techniques for Digital
* Carrier Synchronization", IEEE Aerospace and Electronic Systems Magazine,
* Vol. 32, No. 7, pp. 28–45, July 2017. DOI: 10.1109/MAES.2017.150260
*
* -------------------------------------------------------------------------
*
* Copyright (C) 2010-2018 (see AUTHORS file for a list of contributors)
*
* GNSS-SDR is a software defined Global Navigation
* Satellite Systems receiver
*
* This file is part of GNSS-SDR.
*
* GNSS-SDR is free software: you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation, either version 3 of the License, or
* (at your option) any later version.
*
* GNSS-SDR is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with GNSS-SDR. If not, see <http://www.gnu.org/licenses/>.
*
* -------------------------------------------------------------------------
*/
#ifndef GNSS_SDR_GPS_L1_CA_KF_TRACKING_CC_H
#define GNSS_SDR_GPS_L1_CA_KF_TRACKING_CC_H
#include "gnss_synchro.h"
#include "tracking_2nd_DLL_filter.h"
#include "tracking_2nd_PLL_filter.h"
#include "cpu_multicorrelator_real_codes.h"
#include "bayesian_estimation.h"
#include <armadillo>
#include <gnuradio/block.h>
#include <fstream>
#include <map>
#include <string>
class Gps_L1_Ca_Kf_Tracking_cc;
typedef boost::shared_ptr<Gps_L1_Ca_Kf_Tracking_cc>
gps_l1_ca_kf_tracking_cc_sptr;
gps_l1_ca_kf_tracking_cc_sptr
gps_l1_ca_kf_make_tracking_cc(uint32_t order,
int64_t if_freq,
int64_t fs_in, uint32_t vector_length,
bool dump,
std::string dump_filename,
float pll_bw_hz,
float early_late_space_chips,
bool bce_run,
uint32_t bce_ptrans,
uint32_t bce_strans,
int32_t bce_nu,
int32_t bce_kappa);
/*!
* \brief This class implements a DLL + PLL tracking loop block
*/
class Gps_L1_Ca_Kf_Tracking_cc : public gr::block
{
public:
~Gps_L1_Ca_Kf_Tracking_cc();
void set_channel(uint32_t channel);
void set_gnss_synchro(Gnss_Synchro* p_gnss_synchro);
void start_tracking();
int general_work(int noutput_items, gr_vector_int& ninput_items,
gr_vector_const_void_star& input_items, gr_vector_void_star& output_items);
void forecast(int noutput_items, gr_vector_int& ninput_items_required);
private:
friend gps_l1_ca_kf_tracking_cc_sptr
gps_l1_ca_kf_make_tracking_cc(uint32_t order,
int64_t if_freq,
int64_t fs_in, uint32_t vector_length,
bool dump,
std::string dump_filename,
float dll_bw_hz,
float early_late_space_chips,
bool bce_run,
uint32_t bce_ptrans,
uint32_t bce_strans,
int32_t bce_nu,
int32_t bce_kappa);
Gps_L1_Ca_Kf_Tracking_cc(uint32_t order,
int64_t if_freq,
int64_t fs_in, uint32_t vector_length,
bool dump,
std::string dump_filename,
float dll_bw_hz,
float early_late_space_chips,
bool bce_run,
uint32_t bce_ptrans,
uint32_t bce_strans,
int32_t bce_nu,
int32_t bce_kappa);
// tracking configuration vars
uint32_t d_order;
uint32_t d_vector_length;
bool d_dump;
Gnss_Synchro* d_acquisition_gnss_synchro;
uint32_t d_channel;
int64_t d_if_freq;
int64_t d_fs_in;
double d_early_late_spc_chips;
// remaining code phase and carrier phase between tracking loops
double d_rem_code_phase_samples;
double d_rem_code_phase_chips;
double d_rem_carr_phase_rad;
// Kalman filter variables
arma::mat kf_P_x_ini; // initial state error covariance matrix
arma::mat kf_P_x; // state error covariance matrix
arma::mat kf_P_x_pre; // Predicted state error covariance matrix
arma::mat kf_P_y; // innovation covariance matrix
arma::mat kf_F; // state transition matrix
arma::mat kf_H; // system matrix
arma::mat kf_R; // measurement error covariance matrix
arma::mat kf_Q; // system error covariance matrix
arma::colvec kf_x; // state vector
arma::colvec kf_x_pre; // predicted state vector
arma::colvec kf_y; // measurement vector
arma::mat kf_K; // Kalman gain matrix
// Bayesian estimator
Bayesian_estimator bayes_estimator;
arma::mat kf_R_est; // measurement error covariance
uint32_t bayes_ptrans;
uint32_t bayes_strans;
int32_t bayes_nu;
int32_t bayes_kappa;
bool bayes_run;
uint32_t kf_iter;
// PLL and DLL filter library
Tracking_2nd_DLL_filter d_code_loop_filter;
// Tracking_2nd_PLL_filter d_carrier_loop_filter;
// acquisition
double d_acq_carrier_doppler_step_hz;
double d_acq_code_phase_samples;
double d_acq_carrier_doppler_hz;
// correlator
int32_t d_n_correlator_taps;
float* d_ca_code;
float* d_local_code_shift_chips;
gr_complex* d_correlator_outs;
cpu_multicorrelator_real_codes multicorrelator_cpu;
// tracking vars
double d_code_freq_chips;
double d_code_phase_step_chips;
double d_carrier_doppler_hz;
double d_carrier_dopplerrate_hz2;
double d_carrier_phase_step_rad;
double d_acc_carrier_phase_rad;
double d_carr_phase_error_rad;
double d_carr_phase_sigma2;
double d_code_phase_samples;
double code_error_chips;
double code_error_filt_chips;
// PRN period in samples
int32_t d_current_prn_length_samples;
// processing samples counters
uint64_t d_sample_counter;
uint64_t d_acq_sample_stamp;
// CN0 estimation and lock detector
int32_t d_cn0_estimation_counter;
gr_complex* d_Prompt_buffer;
double d_carrier_lock_test;
double d_CN0_SNV_dB_Hz;
double d_carrier_lock_threshold;
int32_t d_carrier_lock_fail_counter;
// control vars
bool d_enable_tracking;
bool d_pull_in;
// file dump
std::string d_dump_filename;
std::ofstream d_dump_file;
std::map<std::string, std::string> systemName;
std::string sys;
int32_t save_matfile();
};
#endif // GNSS_SDR_GPS_L1_CA_KF_TRACKING_CC_H

2
src/algorithms/tracking/libs/CMakeLists.txt
View File

@ -44,6 +44,7 @@ set(TRACKING_LIB_SOURCES
tracking_FLL_PLL_filter.cc
tracking_loop_filter.cc
dll_pll_conf.cc
bayesian_estimation.cc
)
if(ENABLE_FPGA)
@ -56,6 +57,7 @@ include_directories(
${CMAKE_SOURCE_DIR}/src/core/interfaces
${CMAKE_SOURCE_DIR}/src/core/receiver
${CMAKE_SOURCE_DIR}/src/algorithms/libs
${ARMADILLO_INCLUDE_DIRS}
${VOLK_INCLUDE_DIRS}
${GLOG_INCLUDE_DIRS}
${GFlags_INCLUDE_DIRS}

187
src/algorithms/tracking/libs/bayesian_estimation.cc Normal file
View File

@ -0,0 +1,187 @@
/*!
* \file bayesian_estimation.cc
* \brief Interface of a library with Bayesian noise statistic estimation
*
* Bayesian_estimator is a Bayesian estimator which attempts to estimate
* the properties of a stochastic process based on a sequence of
* discrete samples of the sequence.
*
* [1] TODO: Refs
*
* \authors <ul>
* <li> Gerald LaMountain, 2018. gerald(at)ece.neu.edu
* <li> Jordi Vila-Valls 2018. jvila(at)cttc.es
* </ul>
* -------------------------------------------------------------------------
*
* Copyright (C) 2010-2018 (see AUTHORS file for a list of contributors)
*
* GNSS-SDR is a software defined Global Navigation
* Satellite Systems receiver
*
* This file is part of GNSS-SDR.
*
* GNSS-SDR is free software: you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation, either version 3 of the License, or
* (at your option) any later version.
*
* GNSS-SDR is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with GNSS-SDR. If not, see <https://www.gnu.org/licenses/>.
*
* -------------------------------------------------------------------------
*/
#include "bayesian_estimation.h"
Bayesian_estimator::Bayesian_estimator()
{
int ny = 1;
mu_prior = arma::zeros(ny, 1);
kappa_prior = 0;
nu_prior = 0;
Psi_prior = arma::eye(ny, ny) * (nu_prior + ny + 1);
mu_est = mu_prior;
Psi_est = Psi_prior;
}
Bayesian_estimator::Bayesian_estimator(int ny)
{
mu_prior = arma::zeros(ny, 1);
kappa_prior = 0;
nu_prior = 0;
Psi_prior = arma::eye(ny, ny) * (nu_prior + ny + 1);
mu_est = mu_prior;
Psi_est = Psi_prior;
}
Bayesian_estimator::Bayesian_estimator(const arma::vec& mu_prior_0, int kappa_prior_0, int nu_prior_0, const arma::mat& Psi_prior_0)
{
mu_prior = mu_prior_0;
kappa_prior = kappa_prior_0;
nu_prior = nu_prior_0;
Psi_prior = Psi_prior_0;
mu_est = mu_prior;
Psi_est = Psi_prior;
}
Bayesian_estimator::~Bayesian_estimator()
{
}
void Bayesian_estimator::init(const arma::mat& mu_prior_0, int kappa_prior_0, int nu_prior_0, const arma::mat& Psi_prior_0)
{
mu_prior = mu_prior_0;
kappa_prior = kappa_prior_0;
nu_prior = nu_prior_0;
Psi_prior = Psi_prior_0;
mu_est = mu_prior;
Psi_est = Psi_prior;
}
/*
* Perform Bayesian noise estimation using the normal-inverse-Wishart priors stored in
* the class structure, and update the priors according to the computed posteriors
*/
void Bayesian_estimator::update_sequential(const arma::vec& data)
{
int K = data.n_cols;
int ny = data.n_rows;
if (mu_prior.is_empty())
{
mu_prior = arma::zeros(ny, 1);
}
if (Psi_prior.is_empty())
{
Psi_prior = arma::zeros(ny, ny);
}
arma::vec y_mean = arma::mean(data, 1);
arma::mat Psi_N = arma::zeros(ny, ny);
for (int kk = 0; kk < K; kk++)
{
Psi_N = Psi_N + (data.col(kk) - y_mean) * ((data.col(kk) - y_mean).t());
}
arma::vec mu_posterior = (kappa_prior * mu_prior + K * y_mean) / (kappa_prior + K);
int kappa_posterior = kappa_prior + K;
int nu_posterior = nu_prior + K;
arma::mat Psi_posterior = Psi_prior + Psi_N + (kappa_prior * K) / (kappa_prior + K) * (y_mean - mu_prior) * ((y_mean - mu_prior).t());
mu_est = mu_posterior;
if ((nu_posterior - ny - 1) > 0)
{
Psi_est = Psi_posterior / (nu_posterior - ny - 1);
}
else
{
Psi_est = Psi_posterior / (nu_posterior + ny + 1);
}
mu_prior = mu_posterior;
kappa_prior = kappa_posterior;
nu_prior = nu_posterior;
Psi_prior = Psi_posterior;
}
/*
* Perform Bayesian noise estimation using a new set of normal-inverse-Wishart priors
* and update the priors according to the computed posteriors
*/
void Bayesian_estimator::update_sequential(const arma::vec& data, const arma::vec& mu_prior_0, int kappa_prior_0, int nu_prior_0, const arma::mat& Psi_prior_0)
{
int K = data.n_cols;
int ny = data.n_rows;
arma::vec y_mean = arma::mean(data, 1);
arma::mat Psi_N = arma::zeros(ny, ny);
for (int kk = 0; kk < K; kk++)
{
Psi_N = Psi_N + (data.col(kk) - y_mean) * ((data.col(kk) - y_mean).t());
}
arma::vec mu_posterior = (kappa_prior_0 * mu_prior_0 + K * y_mean) / (kappa_prior_0 + K);
int kappa_posterior = kappa_prior_0 + K;
int nu_posterior = nu_prior_0 + K;
arma::mat Psi_posterior = Psi_prior_0 + Psi_N + (kappa_prior_0 * K) / (kappa_prior_0 + K) * (y_mean - mu_prior_0) * ((y_mean - mu_prior_0).t());
mu_est = mu_posterior;
if ((nu_posterior - ny - 1) > 0)
{
Psi_est = Psi_posterior / (nu_posterior - ny - 1);
}
else
{
Psi_est = Psi_posterior / (nu_posterior + ny + 1);
}
mu_prior = mu_posterior;
kappa_prior = kappa_posterior;
nu_prior = nu_posterior;
Psi_prior = Psi_posterior;
}
arma::mat Bayesian_estimator::get_mu_est() const
{
return mu_est;
}
arma::mat Bayesian_estimator::get_Psi_est() const
{
return Psi_est;
}

85
src/algorithms/tracking/libs/bayesian_estimation.h Normal file
View File

@ -0,0 +1,85 @@
/*!
* \file bayesian_estimation.h
* \brief Interface of a library with Bayesian noise statistic estimation
*
* Bayesian_estimator is a Bayesian estimator which attempts to estimate
* the properties of a stochastic process based on a sequence of
* discrete samples of the sequence.
*
* [1] TODO: Refs
*
* \authors <ul>
* <li> Gerald LaMountain, 2018. gerald(at)ece.neu.edu
* <li> Jordi Vila-Valls 2018. jvila(at)cttc.es
* </ul>
* -------------------------------------------------------------------------
*
* Copyright (C) 2010-2018 (see AUTHORS file for a list of contributors)
*
* GNSS-SDR is a software defined Global Navigation
* Satellite Systems receiver
*
* This file is part of GNSS-SDR.
*
* GNSS-SDR is free software: you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation, either version 3 of the License, or
* (at your option) any later version.
*
* GNSS-SDR is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with GNSS-SDR. If not, see <https://www.gnu.org/licenses/>.
*
* -------------------------------------------------------------------------
*/
#ifndef GNSS_SDR_BAYESIAN_ESTIMATION_H_
#define GNSS_SDR_BAYESIAN_ESTIMATION_H_
#include <gnuradio/gr_complex.h>
#include <armadillo>
/*! \brief Bayesian_estimator is an estimator of noise characteristics (i.e. mean, covariance)
*
* Bayesian_estimator is an estimator which performs estimation of noise characteristics from
* a sequence of identically and independently distributed (IID) samples of a stationary
* stochastic process by way of Bayesian inference using conjugate priors. The posterior
* distribution is assumed to be Gaussian with mean \mathbf{\mu} and covariance \hat{\mathbf{C}},
* which has a conjugate prior given by a normal-inverse-Wishart distribution with paramemters
* \mathbf{\mu}_{0}, \kappa_{0}, \nu_{0}, and \mathbf{\Psi}.
*
* [1] TODO: Ref1
*
*/
class Bayesian_estimator
{
public:
Bayesian_estimator();
Bayesian_estimator(int ny);
Bayesian_estimator(const arma::vec& mu_prior_0, int kappa_prior_0, int nu_prior_0, const arma::mat& Psi_prior_0);
~Bayesian_estimator();
void init(const arma::mat& mu_prior_0, int kappa_prior_0, int nu_prior_0, const arma::mat& Psi_prior_0);
void update_sequential(const arma::vec& data);
void update_sequential(const arma::vec& data, const arma::vec& mu_prior_0, int kappa_prior_0, int nu_prior_0, const arma::mat& Psi_prior_0);
arma::mat get_mu_est() const;
arma::mat get_Psi_est() const;
private:
arma::vec mu_est;
arma::mat Psi_est;
arma::vec mu_prior;
int kappa_prior;
int nu_prior;
arma::mat Psi_prior;
};
#endif

13
src/core/receiver/gnss_block_factory.cc
View File

@ -104,6 +104,7 @@
#include "sbas_l1_telemetry_decoder.h"
#include "hybrid_observables.h"
#include "rtklib_pvt.h"
#include "gps_l1_ca_kf_tracking.h"
#if RAW_UDP
#include "custom_udp_signal_source.h"
@ -1501,6 +1502,12 @@ std::unique_ptr<GNSSBlockInterface> GNSSBlockFactory::GetBlock(
out_streams));
block = std::move(block_);
}
else if (implementation.compare("GPS_L1_CA_KF_Tracking") == 0)
{
std::unique_ptr<GNSSBlockInterface> block_(new GpsL1CaKfTracking(configuration.get(), role, in_streams,
out_streams));
block = std::move(block_);
}
else if (implementation.compare("GPS_L1_CA_DLL_PLL_C_Aid_Tracking") == 0)
{
std::unique_ptr<TrackingInterface> block_(new GpsL1CaDllPllCAidTracking(configuration.get(), role, in_streams,
@ -1876,6 +1883,12 @@ std::unique_ptr<TrackingInterface> GNSSBlockFactory::GetTrkBlock(
out_streams));
block = std::move(block_);
}
else if (implementation.compare("GPS_L1_CA_KF_Tracking") == 0)
{
std::unique_ptr<TrackingInterface> block_(new GpsL1CaKfTracking(configuration.get(), role, in_streams,
out_streams));
block = std::move(block_);
}
else if (implementation.compare("GPS_L1_CA_DLL_PLL_C_Aid_Tracking") == 0)
{
std::unique_ptr<TrackingInterface> block_(new GpsL1CaDllPllCAidTracking(configuration.get(), role, in_streams,

2
src/core/receiver/gnss_flowgraph.cc
View File

@ -1183,7 +1183,7 @@ void GNSSFlowgraph::set_signals_list()
11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28,
29, 30, 31, 32};
std::set<unsigned int> available_sbas_prn = {120, 124, 126};
std::set<unsigned int> available_sbas_prn = {123, 131, 135, 136, 138};
std::set<unsigned int> available_galileo_prn = {1, 2, 3, 4, 5, 6, 7, 8, 9, 10,
11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28,

2
src/core/system_parameters/GPS_L1_CA.h
View File

@ -54,7 +54,7 @@ const double GPS_L1_FREQ_HZ = FREQ1; //!< L1 [Hz]
const double GPS_L1_CA_CODE_RATE_HZ = 1.023e6; //!< GPS L1 C/A code rate [chips/s]
const double GPS_L1_CA_CODE_LENGTH_CHIPS = 1023.0; //!< GPS L1 C/A code length [chips]
const double GPS_L1_CA_CODE_PERIOD = 0.001; //!< GPS L1 C/A code period [seconds]
const uint32_t GPS_L1_CA_CODE_PERIOD_MS = 1; //!< GPS L1 C/A code period [ms]
const uint32_t GPS_L1_CA_CODE_PERIOD_MS = 1U; //!< GPS L1 C/A code period [ms]
const double GPS_L1_CA_CHIP_PERIOD = 9.7752e-07; //!< GPS L1 C/A chip period [seconds]
/*!

12
src/core/system_parameters/galileo_navigation_message.cc
View File

@ -229,11 +229,11 @@ Galileo_Navigation_Message::Galileo_Navigation_Message()
}
bool Galileo_Navigation_Message::CRC_test(std::bitset<GALILEO_DATA_FRAME_BITS> bits, boost::uint32_t checksum)
bool Galileo_Navigation_Message::CRC_test(std::bitset<GALILEO_DATA_FRAME_BITS> bits, uint32_t checksum)
{
CRC_Galileo_INAV_type CRC_Galileo;
boost::uint32_t crc_computed;
uint32_t crc_computed;
// Galileo INAV frame for CRC is not an integer multiple of bytes
// it needs to be filled with zeroes at the start of the frame.
// This operation is done in the transformation from bits to bytes
@ -290,7 +290,7 @@ uint64_t Galileo_Navigation_Message::read_page_type_unsigned(std::bitset<GALILEO
value <<= 1; // shift left
if (bits[GALILEO_PAGE_TYPE_BITS - parameter[i].first - j] == 1)
{
value += 1; // insert the bit
value += 1ULL; // insert the bit
}
}
}
@ -306,11 +306,11 @@ int64_t Galileo_Navigation_Message::read_navigation_signed(std::bitset<GALILEO_D
// read the MSB and perform the sign extension
if (bits[GALILEO_DATA_JK_BITS - parameter[0].first] == 1)
{
value ^= 0xFFFFFFFFFFFFFFFF; // 64 bits variable
value ^= 0xFFFFFFFFFFFFFFFFLL; // 64 bits variable
}
else
{
value &= 0;
value &= 0LL;
}
for (int32_t i = 0; i < num_of_slices; i++)
@ -321,7 +321,7 @@ int64_t Galileo_Navigation_Message::read_navigation_signed(std::bitset<GALILEO_D
value &= 0xFFFFFFFFFFFFFFFE; // reset the corresponding bit (for the 64 bits variable)
if (bits[GALILEO_DATA_JK_BITS - parameter[i].first - j] == 1)
{
value += 1; // insert the bit
value += 1LL; // insert the bit
}
}
}

30
src/core/system_parameters/glonass_gnav_navigation_message.cc
View File

@ -236,10 +236,10 @@ uint64_t Glonass_Gnav_Navigation_Message::read_navigation_unsigned(std::bitset<G
{
for (int32_t j = 0; j < parameter[i].second; j++)
{
value <<= 1; //shift left
value <<= 1; // shift left
if (bits[GLONASS_GNAV_STRING_BITS - parameter[i].first - j] == 1)
{
value += 1; // insert the bit
value += 1ULL; // insert the bit
}
}
}
@ -255,20 +255,20 @@ int64_t Glonass_Gnav_Navigation_Message::read_navigation_signed(std::bitset<GLON
// read the MSB and perform the sign extension
if (bits[GLONASS_GNAV_STRING_BITS - parameter[0].first] == 1)
{
sign = -1;
sign = -1LL;
}
else
{
sign = 1;
sign = 1LL;
}
for (int32_t i = 0; i < num_of_slices; i++)
{
for (int32_t j = 1; j < parameter[i].second; j++)
{
value <<= 1; //shift left
value <<= 1; // shift left
if (bits[GLONASS_GNAV_STRING_BITS - parameter[i].first - j] == 1)
{
value += 1; // insert the bit
value += 1LL; // insert the bit
}
}
}
@ -278,32 +278,32 @@ int64_t Glonass_Gnav_Navigation_Message::read_navigation_signed(std::bitset<GLON
uint32_t Glonass_Gnav_Navigation_Message::get_frame_number(uint32_t satellite_slot_number)
{
uint32_t frame_ID = 0;
uint32_t frame_ID = 0U;
if (satellite_slot_number >= 1 and satellite_slot_number <= 5)
{
frame_ID = 1;
frame_ID = 1U;
}
else if (satellite_slot_number >= 6 and satellite_slot_number <= 10)
{
frame_ID = 2;
frame_ID = 2U;
}
else if (satellite_slot_number >= 11 and satellite_slot_number <= 15)
{
frame_ID = 3;
frame_ID = 3U;
}
else if (satellite_slot_number >= 16 and satellite_slot_number <= 20)
{
frame_ID = 4;
frame_ID = 4U;
}
else if (satellite_slot_number >= 21 and satellite_slot_number <= 24)
{
frame_ID = 5;
frame_ID = 5U;
}
else
{
LOG(WARNING) << "GLONASS GNAV: Invalid Satellite Slot Number";
frame_ID = 0;
frame_ID = 0U;
}
return frame_ID;
@ -313,8 +313,8 @@ uint32_t Glonass_Gnav_Navigation_Message::get_frame_number(uint32_t satellite_sl
int32_t Glonass_Gnav_Navigation_Message::string_decoder(std::string frame_string)
{
int32_t J = 0;
d_string_ID = 0;
d_frame_ID = 0;
d_string_ID = 0U;
d_frame_ID = 0U;
// Unpack bytes to bits
std::bitset<GLONASS_GNAV_STRING_BITS> string_bits(frame_string);

49
src/core/system_parameters/gnss_satellite.cc
View File

@ -184,26 +184,30 @@ void Gnss_Satellite::set_PRN(uint32_t PRN_)
}
else if (system.compare("SBAS") == 0)
{
if (PRN_ == 122)
if (PRN_ == 120)
{
PRN = PRN_;
} // WAAS Inmarsat 3F4 (AOR-W)
else if (PRN_ == 134)
} // EGNOS Test Platform.Inmarsat 3-F2 (Atlantic Ocean Region-East)
else if (PRN_ == 123)
{
PRN = PRN_;
} // WAAS Inmarsat 3F3 (POR)
else if (PRN_ == 120)
} // EGNOS Operational Platform. Astra 5B
else if (PRN_ == 131)
{
PRN = PRN_;
} // EGNOS AOR-E Broadcast satellite http://www.egnos-pro.esa.int/index.html
else if (PRN_ == 124)
} // WAAS Eutelsat 117 West B
else if (PRN_ == 135)
{
PRN = PRN_;
} // EGNOS ESA ARTEMIS used for EGNOS Operations
else if (PRN_ == 126)
} // WAAS Galaxy 15
else if (PRN_ == 136)
{
PRN = PRN_;
} // EGNOS IOR-W currently used by Industry to perform various tests on the system.
} // EGNOS Operational Platform. SES-5 (a.k.a. Sirius 5 or Astra 4B)
else if (PRN_ == 138)
{
PRN = PRN_;
} // WAAS Anik F1R
else
{
DLOG(INFO) << "This PRN is not defined";
@ -492,20 +496,23 @@ std::string Gnss_Satellite::what_block(const std::string& system_, uint32_t PRN_
{
switch (PRN_)
{
case 122:
block_ = std::string("WAAS"); // WAAS Inmarsat 3F4 (AOR-W)
break;
case 134:
block_ = std::string("WAAS"); // WAAS Inmarsat 3F3 (POR)
break;
case 120:
block_ = std::string("EGNOS"); // EGNOS AOR-E Broadcast satellite http://www.egnos-pro.esa.int/index.html
block_ = std::string("EGNOS Test Platform"); // Inmarsat 3-F2 (Atlantic Ocean Region-East)
break;
case 124:
block_ = std::string("EGNOS"); // EGNOS ESA ARTEMIS used for EGNOS Operations
case 123:
block_ = std::string("EGNOS"); // EGNOS Operational Platform. Astra 5B
break;
case 126:
block_ = std::string("EGNOS"); // EGNOS IOR-W currently used by Industry to perform various tests on the system.
case 131:
block_ = std::string("WAAS"); // WAAS Eutelsat 117 West B
break;
case 135:
block_ = std::string("WAAS"); // WAAS Galaxy 15
break;
case 136:
block_ = std::string("EGNOS"); // EGNOS Operational Platform. SES-5 (a.k.a. Sirius 5 or Astra 4B)
break;
case 138:
block_ = std::string("WAAS"); // WAAS Anik F1R
break;
default:
block_ = std::string("Unknown");

2
src/core/system_parameters/gnss_synchro.h
View File

@ -53,6 +53,7 @@ public:
double Acq_delay_samples; //!< Set by Acquisition processing block
double Acq_doppler_hz; //!< Set by Acquisition processing block
uint64_t Acq_samplestamp_samples; //!< Set by Acquisition processing block
uint32_t Acq_doppler_step; //!< Set by Acquisition processing block
bool Flag_valid_acquisition; //!< Set by Acquisition processing block
// Tracking
@ -96,6 +97,7 @@ public:
ar& Acq_delay_samples;
ar& Acq_doppler_hz;
ar& Acq_samplestamp_samples;
ar& Acq_doppler_step;
ar& Flag_valid_acquisition;
// Tracking
ar& fs;

10
src/core/system_parameters/gps_cnav_navigation_message.cc
View File

@ -99,7 +99,7 @@ uint64_t Gps_CNAV_Navigation_Message::read_navigation_unsigned(std::bitset<GPS_C
value <<= 1; // shift left
if (bits[GPS_CNAV_DATA_PAGE_BITS - parameter[i].first - j] == 1)
{
value += 1; // insert the bit
value += 1ULL; // insert the bit
}
}
}
@ -115,11 +115,11 @@ int64_t Gps_CNAV_Navigation_Message::read_navigation_signed(std::bitset<GPS_CNAV
// read the MSB and perform the sign extension
if (bits[GPS_CNAV_DATA_PAGE_BITS - parameter[0].first] == 1)
{
value ^= 0xFFFFFFFFFFFFFFFF; // 64 bits variable
value ^= 0xFFFFFFFFFFFFFFFFLL; // 64 bits variable
}
else
{
value &= 0;
value &= 0LL;
}
for (int32_t i = 0; i < num_of_slices; i++)
@ -127,10 +127,10 @@ int64_t Gps_CNAV_Navigation_Message::read_navigation_signed(std::bitset<GPS_CNAV
for (int32_t j = 0; j < parameter[i].second; j++)
{
value <<= 1; // shift left
value &= 0xFFFFFFFFFFFFFFFE; // reset the corresponding bit (for the 64 bits variable)
value &= 0xFFFFFFFFFFFFFFFELL; // reset the corresponding bit (for the 64 bits variable)
if (bits[GPS_CNAV_DATA_PAGE_BITS - parameter[i].first - j] == 1)
{
value += 1; // insert the bit
value += 1LL; // insert the bit
}
}
}

12
src/core/system_parameters/gps_navigation_message.cc
View File

@ -184,10 +184,10 @@ uint64_t Gps_Navigation_Message::read_navigation_unsigned(std::bitset<GPS_SUBFRA
{
for (int32_t j = 0; j < parameter[i].second; j++)
{
value <<= 1; //shift left
value <<= 1; // shift left
if (bits[GPS_SUBFRAME_BITS - parameter[i].first - j] == 1)
{
value += 1; // insert the bit
value += 1ULL; // insert the bit
}
}
}
@ -203,11 +203,11 @@ int64_t Gps_Navigation_Message::read_navigation_signed(std::bitset<GPS_SUBFRAME_
// read the MSB and perform the sign extension
if (bits[GPS_SUBFRAME_BITS - parameter[0].first] == 1)
{
value ^= 0xFFFFFFFFFFFFFFFF; // 64 bits variable
value ^= 0xFFFFFFFFFFFFFFFFLL; // 64 bits variable
}
else
{
value &= 0;
value &= 0LL;
}
for (int32_t i = 0; i < num_of_slices; i++)
@ -215,10 +215,10 @@ int64_t Gps_Navigation_Message::read_navigation_signed(std::bitset<GPS_SUBFRAME_
for (int32_t j = 0; j < parameter[i].second; j++)
{
value <<= 1; // shift left
value &= 0xFFFFFFFFFFFFFFFE; // reset the corresponding bit (for the 64 bits variable)
value &= 0xFFFFFFFFFFFFFFFELL; // reset the corresponding bit (for the 64 bits variable)
if (bits[GPS_SUBFRAME_BITS - parameter[i].first - j] == 1)
{
value += 1; // insert the bit
value += 1LL; // insert the bit
}
}
}

3
src/tests/CMakeLists.txt
View File

@ -666,7 +666,8 @@ endif(NOT ${GTEST_DIR_LOCAL})
add_executable(trk_test ${CMAKE_CURRENT_SOURCE_DIR}/single_test_main.cc
${CMAKE_CURRENT_SOURCE_DIR}/unit-tests/signal-processing-blocks/tracking/galileo_e1_dll_pll_veml_tracking_test.cc
${CMAKE_CURRENT_SOURCE_DIR}/unit-tests/signal-processing-blocks/tracking/tracking_loop_filter_test.cc
${CMAKE_CURRENT_SOURCE_DIR}/unit-tests/signal-processing-blocks/tracking/cpu_multicorrelator_real_codes_test.cc )
${CMAKE_CURRENT_SOURCE_DIR}/unit-tests/signal-processing-blocks/tracking/cpu_multicorrelator_real_codes_test.cc
${CMAKE_CURRENT_SOURCE_DIR}/unit-tests/signal-processing-blocks/tracking/bayesian_estimation_test.cc )
target_link_libraries(trk_test ${Boost_LIBRARIES}
${GFlags_LIBS}

2
src/tests/test_main.cc
View File

@ -127,6 +127,7 @@ DECLARE_string(log_dir);
#include "unit-tests/signal-processing-blocks/tracking/tracking_loop_filter_test.cc"
#include "unit-tests/signal-processing-blocks/tracking/cpu_multicorrelator_test.cc"
#include "unit-tests/signal-processing-blocks/tracking/cpu_multicorrelator_real_codes_test.cc"
#include "unit-tests/signal-processing-blocks/tracking/bayesian_estimation_test.cc"
#if CUDA_BLOCKS_TEST
#include "unit-tests/signal-processing-blocks/tracking/gpu_multicorrelator_test.cc"
@ -148,6 +149,7 @@ DECLARE_string(log_dir);
#include "unit-tests/signal-processing-blocks/acquisition/acq_performance_test.cc"
#include "unit-tests/signal-processing-blocks/tracking/gps_l2_m_dll_pll_tracking_test.cc"
#include "unit-tests/signal-processing-blocks/tracking/gps_l1_ca_dll_pll_tracking_test.cc"
#include "unit-tests/signal-processing-blocks/tracking/gps_l1_ca_kf_tracking_test.cc"
#include "unit-tests/signal-processing-blocks/tracking/tracking_pull-in_test.cc"
#if ENABLE_FPGA
#include "unit-tests/signal-processing-blocks/tracking/tracking_pull-in_test_fpga.cc"

69
src/tests/unit-tests/signal-processing-blocks/tracking/bayesian_estimation_test.cc Normal file
View File

@ -0,0 +1,69 @@
/*!
* \file bayesian_estimation_positivity_test.cc
* \brief This file implements timing tests for the Bayesian covariance estimator
* \author Gerald LaMountain, 20168. gerald(at)ece.neu.edu
*
*
* -------------------------------------------------------------------------
*
* Copyright (C) 2010-2018 (see AUTHORS file for a list of contributors)
*
* GNSS-SDR is a software defined Global Navigation
* Satellite Systems receiver
*
* This file is part of GNSS-SDR.
*
* GNSS-SDR is free software: you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation, either version 3 of the License, or
* (at your option) any later version.
*
* GNSS-SDR is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with GNSS-SDR. If not, see <https://www.gnu.org/licenses/>.
*
* -------------------------------------------------------------------------
*/
#include <random>
#include <armadillo>
#include <gtest/gtest.h>
#include "bayesian_estimation.h"
#define BAYESIAN_TEST_N_TRIALS 100
#define BAYESIAN_TEST_ITER 10000
TEST(BayesianEstimationPositivityTest, BayesianPositivityTest)
{
Bayesian_estimator bayes;
arma::vec bayes_mu = arma::zeros(1, 1);
int bayes_nu = 0;
int bayes_kappa = 0;
arma::mat bayes_Psi = arma::ones(1, 1);
arma::vec input = arma::zeros(1, 1);
//--- Perform initializations ------------------------------
std::random_device r;
std::default_random_engine e1(r());
std::normal_distribution<float> normal_dist(0, 5);
for (int k = 0; k < BAYESIAN_TEST_N_TRIALS; k++)
{
bayes.init(bayes_mu, bayes_kappa, bayes_nu, bayes_Psi);
for (int n = 0; n < BAYESIAN_TEST_ITER; n++)
{
input(0) = static_cast<double>(normal_dist(e1));
bayes.update_sequential(input);
arma::mat output = bayes.get_Psi_est();
double output0 = output(0, 0);
ASSERT_EQ(output0 > 0.0, true);
}
}
}

568
src/tests/unit-tests/signal-processing-blocks/tracking/gps_l1_ca_kf_tracking_test.cc Normal file
View File

@ -0,0 +1,568 @@
/*!
* \file gps_l1_ca_kf_tracking_test.cc
* \brief This class implements a tracking test for GPS_L1_CA_KF_Tracking
* implementation based on some input parameters.
* \author Carles Fernandez, 2018
*
*
* -------------------------------------------------------------------------
*
* Copyright (C) 2012-2018 (see AUTHORS file for a list of contributors)
*
* GNSS-SDR is a software defined Global Navigation
* Satellite Systems receiver
*
* This file is part of GNSS-SDR.
*
* GNSS-SDR is free software: you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation, either version 3 of the License, or
* (at your option) any later version.
*
* GNSS-SDR is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with GNSS-SDR. If not, see <http://www.gnu.org/licenses/>.
*
* -------------------------------------------------------------------------
*/
#include <chrono>
#include <unistd.h>
#include <vector>
#include <armadillo>
#include <boost/filesystem.hpp>
#include <gnuradio/top_block.h>
#include <gnuradio/blocks/file_source.h>
#include <gnuradio/analog/sig_source_waveform.h>
#include <gnuradio/analog/sig_source_c.h>
#include <gnuradio/blocks/interleaved_char_to_complex.h>
#include <gnuradio/blocks/null_sink.h>
#include <gnuradio/blocks/skiphead.h>
#include <gtest/gtest.h>
#include "GPS_L1_CA.h"
#include "gnss_block_factory.h"
#include "tracking_interface.h"
#include "in_memory_configuration.h"
#include "tracking_true_obs_reader.h"
#include "tracking_dump_reader.h"
#include "signal_generator_flags.h"
#include "gnuplot_i.h"
#include "test_flags.h"
#include "gnss_sdr_flags.h"
DEFINE_bool(plot_gps_l1_kf_tracking_test, false, "Plots results of GpsL1CAKfTrackingTest with gnuplot");
// ######## GNURADIO BLOCK MESSAGE RECEVER #########
class GpsL1CAKfTrackingTest_msg_rx;
typedef boost::shared_ptr<GpsL1CAKfTrackingTest_msg_rx> GpsL1CAKfTrackingTest_msg_rx_sptr;
GpsL1CAKfTrackingTest_msg_rx_sptr GpsL1CAKfTrackingTest_msg_rx_make();
class GpsL1CAKfTrackingTest_msg_rx : public gr::block
{
private:
friend GpsL1CAKfTrackingTest_msg_rx_sptr GpsL1CAKfTrackingTest_msg_rx_make();
void msg_handler_events(pmt::pmt_t msg);
GpsL1CAKfTrackingTest_msg_rx();
public:
int rx_message;
~GpsL1CAKfTrackingTest_msg_rx(); //!< Default destructor
};
GpsL1CAKfTrackingTest_msg_rx_sptr GpsL1CAKfTrackingTest_msg_rx_make()
{
return GpsL1CAKfTrackingTest_msg_rx_sptr(new GpsL1CAKfTrackingTest_msg_rx());
}
void GpsL1CAKfTrackingTest_msg_rx::msg_handler_events(pmt::pmt_t msg)
{
try
{
long int message = pmt::to_long(msg);
rx_message = message;
}
catch (boost::bad_any_cast& e)
{
LOG(WARNING) << "msg_handler_telemetry Bad any cast!";
rx_message = 0;
}
}
GpsL1CAKfTrackingTest_msg_rx::GpsL1CAKfTrackingTest_msg_rx() : gr::block("GpsL1CAKfTrackingTest_msg_rx", gr::io_signature::make(0, 0, 0), gr::io_signature::make(0, 0, 0))
{
this->message_port_register_in(pmt::mp("events"));
this->set_msg_handler(pmt::mp("events"), boost::bind(&GpsL1CAKfTrackingTest_msg_rx::msg_handler_events, this, _1));
rx_message = 0;
}
GpsL1CAKfTrackingTest_msg_rx::~GpsL1CAKfTrackingTest_msg_rx()
{
}
// ###########################################################
class GpsL1CAKfTrackingTest : public ::testing::Test
{
public:
std::string generator_binary;
std::string p1;
std::string p2;
std::string p3;
std::string p4;
std::string p5;
std::string implementation = "GPS_L1_CA_KF_Tracking";
const int baseband_sampling_freq = FLAGS_fs_gen_sps;
std::string filename_rinex_obs = FLAGS_filename_rinex_obs;
std::string filename_raw_data = FLAGS_filename_raw_data;
int configure_generator();
int generate_signal();
void check_results_doppler(arma::vec& true_time_s,
arma::vec& true_value,
arma::vec& meas_time_s,
arma::vec& meas_value);
void check_results_acc_carrier_phase(arma::vec& true_time_s,
arma::vec& true_value,
arma::vec& meas_time_s,
arma::vec& meas_value);
void check_results_codephase(arma::vec& true_time_s,
arma::vec& true_value,
arma::vec& meas_time_s,
arma::vec& meas_value);
GpsL1CAKfTrackingTest()
{
factory = std::make_shared<GNSSBlockFactory>();
config = std::make_shared<InMemoryConfiguration>();
item_size = sizeof(gr_complex);
gnss_synchro = Gnss_Synchro();
}
~GpsL1CAKfTrackingTest()
{
}
void configure_receiver();
gr::top_block_sptr top_block;
std::shared_ptr<GNSSBlockFactory> factory;
std::shared_ptr<InMemoryConfiguration> config;
Gnss_Synchro gnss_synchro;
size_t item_size;
};
int GpsL1CAKfTrackingTest::configure_generator()
{
// Configure signal generator
generator_binary = FLAGS_generator_binary;
p1 = std::string("-rinex_nav_file=") + FLAGS_rinex_nav_file;
if (FLAGS_dynamic_position.empty())
{
p2 = std::string("-static_position=") + FLAGS_static_position + std::string(",") + std::to_string(FLAGS_duration * 10);
}
else
{
p2 = std::string("-obs_pos_file=") + std::string(FLAGS_dynamic_position);
}
p3 = std::string("-rinex_obs_file=") + FLAGS_filename_rinex_obs; // RINEX 2.10 observation file output
p4 = std::string("-sig_out_file=") + FLAGS_filename_raw_data; // Baseband signal output file. Will be stored in int8_t IQ multiplexed samples
p5 = std::string("-sampling_freq=") + std::to_string(baseband_sampling_freq); // Baseband sampling frequency [MSps]
return 0;
}
int GpsL1CAKfTrackingTest::generate_signal()
{
int child_status;
char* const parmList[] = {&generator_binary[0], &generator_binary[0], &p1[0], &p2[0], &p3[0], &p4[0], &p5[0], NULL};
int pid;
if ((pid = fork()) == -1)
perror("fork err");
else if (pid == 0)
{
execv(&generator_binary[0], parmList);
std::cout << "Return not expected. Must be an execv err." << std::endl;
std::terminate();
}
waitpid(pid, &child_status, 0);
std::cout << "Signal and Observables RINEX and RAW files created." << std::endl;
return 0;
}
void GpsL1CAKfTrackingTest::configure_receiver()
{
gnss_synchro.Channel_ID = 0;
gnss_synchro.System = 'G';
std::string signal = "1C";
signal.copy(gnss_synchro.Signal, 2, 0);
gnss_synchro.PRN = FLAGS_test_satellite_PRN;
config->set_property("GNSS-SDR.internal_fs_sps", std::to_string(baseband_sampling_freq));
// Set Tracking
config->set_property("Tracking_1C.implementation", implementation);
config->set_property("Tracking_1C.item_type", "gr_complex");
if (FLAGS_dll_bw_hz != 0.0)
{
config->set_property("Tracking_1C.dll_bw_hz", std::to_string(FLAGS_dll_bw_hz));
}
else
{
config->set_property("Tracking_1C.dll_bw_hz", "2.0");
}
config->set_property("Tracking_1C.early_late_space_chips", "0.5");
config->set_property("Tracking_1C.extend_correlation_ms", "1");
config->set_property("Tracking_1C.dump", "true");
config->set_property("Tracking_1C.dump_filename", "./tracking_ch_");
}
void GpsL1CAKfTrackingTest::check_results_doppler(arma::vec& true_time_s,
arma::vec& true_value,
arma::vec& meas_time_s,
arma::vec& meas_value)
{
// 1. True value interpolation to match the measurement times
arma::vec true_value_interp;
arma::uvec true_time_s_valid = find(true_time_s > 0);
true_time_s = true_time_s(true_time_s_valid);
true_value = true_value(true_time_s_valid);
arma::uvec meas_time_s_valid = find(meas_time_s > 0);
meas_time_s = meas_time_s(meas_time_s_valid);
meas_value = meas_value(meas_time_s_valid);
arma::interp1(true_time_s, true_value, meas_time_s, true_value_interp);
// 2. RMSE
arma::vec err;
err = meas_value - true_value_interp;
arma::vec err2 = arma::square(err);
double rmse = sqrt(arma::mean(err2));
// 3. Mean err and variance
double error_mean = arma::mean(err);
double error_var = arma::var(err);
// 4. Peaks
double max_error = arma::max(err);
double min_error = arma::min(err);
// 5. report
std::streamsize ss = std::cout.precision();
std::cout << std::setprecision(10) << "TRK Doppler RMSE=" << rmse
<< ", mean=" << error_mean
<< ", stdev=" << sqrt(error_var) << " (max,min)=" << max_error << "," << min_error << " [Hz]" << std::endl;
std::cout.precision(ss);
}
void GpsL1CAKfTrackingTest::check_results_acc_carrier_phase(arma::vec& true_time_s,
arma::vec& true_value,
arma::vec& meas_time_s,
arma::vec& meas_value)
{
// 1. True value interpolation to match the measurement times
arma::vec true_value_interp;
arma::uvec true_time_s_valid = find(true_time_s > 0);
true_time_s = true_time_s(true_time_s_valid);
true_value = true_value(true_time_s_valid);
arma::uvec meas_time_s_valid = find(meas_time_s > 0);
meas_time_s = meas_time_s(meas_time_s_valid);
meas_value = meas_value(meas_time_s_valid);
arma::interp1(true_time_s, true_value, meas_time_s, true_value_interp);
// 2. RMSE
arma::vec err;
err = meas_value - true_value_interp;
arma::vec err2 = arma::square(err);
double rmse = sqrt(arma::mean(err2));
// 3. Mean err and variance
double error_mean = arma::mean(err);
double error_var = arma::var(err);
// 4. Peaks
double max_error = arma::max(err);
double min_error = arma::min(err);
// 5. report
std::streamsize ss = std::cout.precision();
std::cout << std::setprecision(10) << "TRK acc carrier phase RMSE=" << rmse
<< ", mean=" << error_mean
<< ", stdev=" << sqrt(error_var) << " (max,min)=" << max_error << "," << min_error << " [Hz]" << std::endl;
std::cout.precision(ss);
}
void GpsL1CAKfTrackingTest::check_results_codephase(arma::vec& true_time_s,
arma::vec& true_value,
arma::vec& meas_time_s,
arma::vec& meas_value)
{
// 1. True value interpolation to match the measurement times
arma::vec true_value_interp;
arma::uvec true_time_s_valid = find(true_time_s > 0);
true_time_s = true_time_s(true_time_s_valid);
true_value = true_value(true_time_s_valid);
arma::uvec meas_time_s_valid = find(meas_time_s > 0);
meas_time_s = meas_time_s(meas_time_s_valid);
meas_value = meas_value(meas_time_s_valid);
arma::interp1(true_time_s, true_value, meas_time_s, true_value_interp);
// 2. RMSE
arma::vec err;
err = meas_value - true_value_interp;
arma::vec err2 = arma::square(err);
double rmse = sqrt(arma::mean(err2));
// 3. Mean err and variance
double error_mean = arma::mean(err);
double error_var = arma::var(err);
// 4. Peaks
double max_error = arma::max(err);
double min_error = arma::min(err);
// 5. report
std::streamsize ss = std::cout.precision();
std::cout << std::setprecision(10) << "TRK code phase RMSE=" << rmse
<< ", mean=" << error_mean
<< ", stdev=" << sqrt(error_var) << " (max,min)=" << max_error << "," << min_error << " [Chips]" << std::endl;
std::cout.precision(ss);
}
TEST_F(GpsL1CAKfTrackingTest, ValidationOfResults)
{
// Configure the signal generator
configure_generator();
// Generate signal raw signal samples and observations RINEX file
if (FLAGS_disable_generator == false)
{
generate_signal();
}
std::chrono::time_point<std::chrono::system_clock> start, end;
configure_receiver();
// open true observables log file written by the simulator
tracking_true_obs_reader true_obs_data;
int test_satellite_PRN = FLAGS_test_satellite_PRN;
std::cout << "Testing satellite PRN=" << test_satellite_PRN << std::endl;
std::string true_obs_file = std::string("./gps_l1_ca_obs_prn");
true_obs_file.append(std::to_string(test_satellite_PRN));
true_obs_file.append(".dat");
ASSERT_EQ(true_obs_data.open_obs_file(true_obs_file), true) << "Failure opening true observables file";
top_block = gr::make_top_block("Tracking test");
std::shared_ptr<GNSSBlockInterface> trk_ = factory->GetBlock(config, "Tracking_1C", implementation, 1, 1);
std::shared_ptr<TrackingInterface> tracking = std::dynamic_pointer_cast<TrackingInterface>(trk_); //std::make_shared<GpsL1CaDllPllCAidTracking>(config.get(), "Tracking_1C", 1, 1);
boost::shared_ptr<GpsL1CAKfTrackingTest_msg_rx> msg_rx = GpsL1CAKfTrackingTest_msg_rx_make();
// load acquisition data based on the first epoch of the true observations
ASSERT_EQ(true_obs_data.read_binary_obs(), true)
<< "Failure reading true tracking dump file." << std::endl
<< "Maybe sat PRN #" + std::to_string(FLAGS_test_satellite_PRN) +
" is not available?";
// restart the epoch counter
true_obs_data.restart();
std::cout << "Initial Doppler [Hz]=" << true_obs_data.doppler_l1_hz << " Initial code delay [Chips]=" << true_obs_data.prn_delay_chips << std::endl;
gnss_synchro.Acq_delay_samples = (GPS_L1_CA_CODE_LENGTH_CHIPS - true_obs_data.prn_delay_chips / GPS_L1_CA_CODE_LENGTH_CHIPS) * baseband_sampling_freq * GPS_L1_CA_CODE_PERIOD;
gnss_synchro.Acq_doppler_hz = true_obs_data.doppler_l1_hz;
gnss_synchro.Acq_samplestamp_samples = 0;
ASSERT_NO_THROW({
tracking->set_channel(gnss_synchro.Channel_ID);
}) << "Failure setting channel.";
ASSERT_NO_THROW({
tracking->set_gnss_synchro(&gnss_synchro);
}) << "Failure setting gnss_synchro.";
ASSERT_NO_THROW({
tracking->connect(top_block);
}) << "Failure connecting tracking to the top_block.";
ASSERT_NO_THROW({
std::string file = "./" + filename_raw_data;
const char* file_name = file.c_str();
gr::blocks::file_source::sptr file_source = gr::blocks::file_source::make(sizeof(int8_t), file_name, false);
gr::blocks::interleaved_char_to_complex::sptr gr_interleaved_char_to_complex = gr::blocks::interleaved_char_to_complex::make();
gr::blocks::null_sink::sptr sink = gr::blocks::null_sink::make(sizeof(Gnss_Synchro));
top_block->connect(file_source, 0, gr_interleaved_char_to_complex, 0);
top_block->connect(gr_interleaved_char_to_complex, 0, tracking->get_left_block(), 0);
top_block->connect(tracking->get_right_block(), 0, sink, 0);
top_block->msg_connect(tracking->get_right_block(), pmt::mp("events"), msg_rx, pmt::mp("events"));
}) << "Failure connecting the blocks of tracking test.";
tracking->start_tracking();
EXPECT_NO_THROW({
start = std::chrono::system_clock::now();
top_block->run(); // Start threads and wait
end = std::chrono::system_clock::now();
}) << "Failure running the top_block.";
// check results
// load the true values
long int nepoch = true_obs_data.num_epochs();
std::cout << "True observation epochs=" << nepoch << std::endl;
arma::vec true_timestamp_s = arma::zeros(nepoch, 1);
arma::vec true_acc_carrier_phase_cycles = arma::zeros(nepoch, 1);
arma::vec true_Doppler_Hz = arma::zeros(nepoch, 1);
arma::vec true_prn_delay_chips = arma::zeros(nepoch, 1);
arma::vec true_tow_s = arma::zeros(nepoch, 1);
long int epoch_counter = 0;
while (true_obs_data.read_binary_obs())
{
true_timestamp_s(epoch_counter) = true_obs_data.signal_timestamp_s;
true_acc_carrier_phase_cycles(epoch_counter) = true_obs_data.acc_carrier_phase_cycles;
true_Doppler_Hz(epoch_counter) = true_obs_data.doppler_l1_hz;
true_prn_delay_chips(epoch_counter) = true_obs_data.prn_delay_chips;
true_tow_s(epoch_counter) = true_obs_data.tow;
epoch_counter++;
}
//load the measured values
tracking_dump_reader trk_dump;
ASSERT_EQ(trk_dump.open_obs_file(std::string("./tracking_ch_0.dat")), true)
<< "Failure opening tracking dump file";
nepoch = trk_dump.num_epochs();
std::cout << "Measured observation epochs=" << nepoch << std::endl;
//trk_dump.restart();
arma::vec trk_timestamp_s = arma::zeros(nepoch, 1);
arma::vec trk_acc_carrier_phase_cycles = arma::zeros(nepoch, 1);
arma::vec trk_Doppler_Hz = arma::zeros(nepoch, 1);
arma::vec trk_prn_delay_chips = arma::zeros(nepoch, 1);
std::vector<double> prompt;
std::vector<double> early;
std::vector<double> late;
std::vector<double> promptI;
std::vector<double> promptQ;
epoch_counter = 0;
while (trk_dump.read_binary_obs())
{
trk_timestamp_s(epoch_counter) = static_cast<double>(trk_dump.PRN_start_sample_count) / static_cast<double>(baseband_sampling_freq);
trk_acc_carrier_phase_cycles(epoch_counter) = trk_dump.acc_carrier_phase_rad / GPS_TWO_PI;
trk_Doppler_Hz(epoch_counter) = trk_dump.carrier_doppler_hz;
double delay_chips = GPS_L1_CA_CODE_LENGTH_CHIPS - GPS_L1_CA_CODE_LENGTH_CHIPS * (fmod((static_cast<double>(trk_dump.PRN_start_sample_count) + trk_dump.aux1) / static_cast<double>(baseband_sampling_freq), 1.0e-3) / 1.0e-3);
trk_prn_delay_chips(epoch_counter) = delay_chips;
epoch_counter++;
prompt.push_back(trk_dump.abs_P);
early.push_back(trk_dump.abs_E);
late.push_back(trk_dump.abs_L);
promptI.push_back(trk_dump.prompt_I);
promptQ.push_back(trk_dump.prompt_Q);
}
// Align initial measurements and cut the tracking pull-in transitory
double pull_in_offset_s = 1.0;
arma::uvec initial_meas_point = arma::find(trk_timestamp_s >= (true_timestamp_s(0) + pull_in_offset_s), 1, "first");
trk_timestamp_s = trk_timestamp_s.subvec(initial_meas_point(0), trk_timestamp_s.size() - 1);
trk_acc_carrier_phase_cycles = trk_acc_carrier_phase_cycles.subvec(initial_meas_point(0), trk_acc_carrier_phase_cycles.size() - 1);
trk_Doppler_Hz = trk_Doppler_Hz.subvec(initial_meas_point(0), trk_Doppler_Hz.size() - 1);
trk_prn_delay_chips = trk_prn_delay_chips.subvec(initial_meas_point(0), trk_prn_delay_chips.size() - 1);
check_results_doppler(true_timestamp_s, true_Doppler_Hz, trk_timestamp_s, trk_Doppler_Hz);
check_results_codephase(true_timestamp_s, true_prn_delay_chips, trk_timestamp_s, trk_prn_delay_chips);
check_results_acc_carrier_phase(true_timestamp_s, true_acc_carrier_phase_cycles, trk_timestamp_s, trk_acc_carrier_phase_cycles);
std::chrono::duration<double> elapsed_seconds = end - start;
std::cout << "Signal tracking completed in " << elapsed_seconds.count() << " seconds." << std::endl;
if (FLAGS_plot_gps_l1_kf_tracking_test == true)
{
const std::string gnuplot_executable(FLAGS_gnuplot_executable);
if (gnuplot_executable.empty())
{
std::cout << "WARNING: Although the flag plot_gps_l1_tracking_test has been set to TRUE," << std::endl;
std::cout << "gnuplot has not been found in your system." << std::endl;
std::cout << "Test results will not be plotted." << std::endl;
}
else
{
try
{
boost::filesystem::path p(gnuplot_executable);
boost::filesystem::path dir = p.parent_path();
std::string gnuplot_path = dir.native();
Gnuplot::set_GNUPlotPath(gnuplot_path);
std::vector<double> timevec;
double t = 0.0;
for (auto it = prompt.begin(); it != prompt.end(); it++)
{
timevec.push_back(t);
t = t + GPS_L1_CA_CODE_PERIOD;
}
Gnuplot g1("linespoints");
g1.set_title("GPS L1 C/A signal tracking correlators' output (satellite PRN #" + std::to_string(FLAGS_test_satellite_PRN) + ")");
g1.set_grid();
g1.set_xlabel("Time [s]");
g1.set_ylabel("Correlators' output");
g1.cmd("set key box opaque");
unsigned int decimate = static_cast<unsigned int>(FLAGS_plot_decimate);
g1.plot_xy(timevec, prompt, "Prompt", decimate);
g1.plot_xy(timevec, early, "Early", decimate);
g1.plot_xy(timevec, late, "Late", decimate);
g1.savetops("Correlators_outputs");
g1.savetopdf("Correlators_outputs", 18);
g1.showonscreen(); // window output
Gnuplot g2("points");
g2.set_title("Constellation diagram (satellite PRN #" + std::to_string(FLAGS_test_satellite_PRN) + ")");
g2.set_grid();
g2.set_xlabel("Inphase");
g2.set_ylabel("Quadrature");
g2.cmd("set size ratio -1");
g2.plot_xy(promptI, promptQ);
g2.savetops("Constellation");
g2.savetopdf("Constellation", 18);
g2.showonscreen(); // window output
}
catch (const GnuplotException& ge)
{
std::cout << ge.what() << std::endl;
}
}
}
}

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% Reads GNSS-SDR Tracking dump binary file using the provided
% function and plots some internal variables
% Javier Arribas, 2011. jarribas(at)cttc.es
% -------------------------------------------------------------------------
%
% Copyright (C) 2010-2018 (see AUTHORS file for a list of contributors)
%
% GNSS-SDR is a software defined Global Navigation
% Satellite Systems receiver
%
% This file is part of GNSS-SDR.
%
% GNSS-SDR is free software: you can redistribute it and/or modify
% it under the terms of the GNU General Public License as published by
% the Free Software Foundation, either version 3 of the License, or
% at your option) any later version.
%
% GNSS-SDR is distributed in the hope that it will be useful,
% but WITHOUT ANY WARRANTY; without even the implied warranty of
% MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
% GNU General Public License for more details.
%
% You should have received a copy of the GNU General Public License
% along with GNSS-SDR. If not, see <https://www.gnu.org/licenses/>.
%
% -------------------------------------------------------------------------
%
close all;
clear all;
if ~exist('dll_pll_veml_read_tracking_dump.m', 'file')
addpath('./libs')
end
samplingFreq = 6625000; %[Hz]
channels = 8;
first_channel = 0;
code_period = 0.001;
path = '/archive/'; %% CHANGE THIS PATH
figpath = [path];
for N=1:1:channels
tracking_log_path = [path 'epl_tracking_ch_' num2str(N+first_channel-1) '.dat']; %% CHANGE epl_tracking_ch_ BY YOUR dump_filename
GNSS_tracking(N) = gps_l1_ca_kf_read_tracking_dump(tracking_log_path);
end
% GNSS-SDR format conversion to MATLAB GPS receiver
for N=1:1:channels
trackResults(N).status = 'T'; %fake track
trackResults(N).codeFreq = GNSS_tracking(N).code_freq_hz.';
trackResults(N).carrFreq = GNSS_tracking(N).carrier_doppler_hz.';
trackResults(N).carrFreqRate = GNSS_tracking(N).carrier_dopplerrate_hz2.';
trackResults(N).dllDiscr = GNSS_tracking(N).code_error.';
trackResults(N).dllDiscrFilt = GNSS_tracking(N).code_nco.';
trackResults(N).pllDiscr = GNSS_tracking(N).carr_error.';
trackResults(N).pllDiscrFilt = GNSS_tracking(N).carr_nco.';
trackResults(N).I_P = GNSS_tracking(N).prompt_I.';
trackResults(N).Q_P = GNSS_tracking(N).prompt_Q.';
trackResults(N).I_E = GNSS_tracking(N).E.';
trackResults(N).I_L = GNSS_tracking(N).L.';
trackResults(N).Q_E = zeros(1,length(GNSS_tracking(N).E));
trackResults(N).Q_L = zeros(1,length(GNSS_tracking(N).E));
trackResults(N).PRN = GNSS_tracking(N).PRN.';
trackResults(N).CNo = GNSS_tracking(N).CN0_SNV_dB_Hz.';
kalmanResults(N).PRN = GNSS_tracking(N).PRN.';
kalmanResults(N).innovation = GNSS_tracking(N).carr_error.';
kalmanResults(N).state1 = GNSS_tracking(N).carr_nco.';
kalmanResults(N).state2 = GNSS_tracking(N).carrier_doppler_hz.';
kalmanResults(N).state3 = GNSS_tracking(N).carrier_dopplerrate_hz2.';
kalmanResults(N).r_noise_cov = GNSS_tracking(N).carr_noise_sigma2.';
kalmanResults(N).CNo = GNSS_tracking(N).CN0_SNV_dB_Hz.';
% Use original MATLAB tracking plot function
settings.numberOfChannels = channels;
settings.msToProcess = length(GNSS_tracking(N).E);
settings.codePeriod = code_period;
settings.timeStartInSeconds = 20;
%plotTracking(N, trackResults, settings)
plotKalman(N, kalmanResults, settings)
saveas(gcf, [figpath 'epl_tracking_ch_' num2str(N) '_PRN_' num2str(trackResults(N).PRN(end)) '.png'], 'png')
end

158
src/utils/matlab/libs/gps_l1_ca_kf_read_tracking_dump.m Normal file
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% Usage: gps_l1_ca_kf_read_tracking_dump (filename, [count])
%
% Opens GNSS-SDR tracking binary log file .dat and returns the contents
% Read GNSS-SDR Tracking dump binary file into MATLAB.
% Javier Arribas, 2011. jarribas(at)cttc.es
% -------------------------------------------------------------------------
%
% Copyright (C) 2010-2018 (see AUTHORS file for a list of contributors)
%
% GNSS-SDR is a software defined Global Navigation
% Satellite Systems receiver
%
% This file is part of GNSS-SDR.
%
% GNSS-SDR is free software: you can redistribute it and/or modify
% it under the terms of the GNU General Public License as published by
% the Free Software Foundation, either version 3 of the License, or
% at your option) any later version.
%
% GNSS-SDR is distributed in the hope that it will be useful,
% but WITHOUT ANY WARRANTY; without even the implied warranty of
% MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
% GNU General Public License for more details.
%
% You should have received a copy of the GNU General Public License
% along with GNSS-SDR. If not, see <https://www.gnu.org/licenses/>.
%
% -------------------------------------------------------------------------
%
function [GNSS_tracking] = gps_l1_ca_kf_read_tracking_dump (filename, count)
m = nargchk (1,2,nargin);
num_float_vars = 19;
num_unsigned_long_int_vars = 1;
num_double_vars = 1;
num_unsigned_int_vars = 1;
if(~isempty(strfind(computer('arch'), '64')))
% 64-bit computer
double_size_bytes = 8;
unsigned_long_int_size_bytes = 8;
float_size_bytes = 4;
unsigned_int_size_bytes = 4;
else
double_size_bytes = 8;
unsigned_long_int_size_bytes = 4;
float_size_bytes = 4;
unsigned_int_size_bytes = 4;
end
skip_bytes_each_read = float_size_bytes * num_float_vars + unsigned_long_int_size_bytes * num_unsigned_long_int_vars + ...
double_size_bytes * num_double_vars + num_unsigned_int_vars*unsigned_int_size_bytes;
bytes_shift = 0;
if (m)
usage (m);
end
if (nargin < 2)
count = Inf;
end
%loops_counter = fread (f, count, 'uint32',4*12);
f = fopen (filename, 'rb');
if (f < 0)
else
v1 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v2 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v3 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v4 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v5 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v6 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v7 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next interleaved float
v8 = fread (f, count, 'long', skip_bytes_each_read - unsigned_long_int_size_bytes);
bytes_shift = bytes_shift + unsigned_long_int_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v9 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v10 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v11 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v12 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v13 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v14 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v15 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v16 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v17 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v18 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next interleaved float
v19 = fread (f, count, 'float', skip_bytes_each_read - float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next float
v20 = fread (f, count, 'float', skip_bytes_each_read-float_size_bytes);
bytes_shift = bytes_shift + float_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next double
v21 = fread (f, count, 'double', skip_bytes_each_read - double_size_bytes);
bytes_shift = bytes_shift + double_size_bytes;
fseek(f,bytes_shift,'bof'); % move to next unsigned int
v22 = fread (f, count, 'uint', skip_bytes_each_read - unsigned_int_size_bytes);
fclose (f);
GNSS_tracking.VE = v1;
GNSS_tracking.E = v2;
GNSS_tracking.P = v3;
GNSS_tracking.L = v4;
GNSS_tracking.VL = v5;
GNSS_tracking.prompt_I = v6;
GNSS_tracking.prompt_Q = v7;
GNSS_tracking.PRN_start_sample = v8;
GNSS_tracking.acc_carrier_phase_rad = v9;
GNSS_tracking.carrier_doppler_hz = v10;
GNSS_tracking.carrier_dopplerrate_hz2 = v11;
GNSS_tracking.code_freq_hz = v12;
GNSS_tracking.carr_error = v13;
GNSS_tracking.carr_noise_sigma2 = v14;
GNSS_tracking.carr_nco = v15;
GNSS_tracking.code_error = v16;
GNSS_tracking.code_nco = v17;
GNSS_tracking.CN0_SNV_dB_Hz = v18;
GNSS_tracking.carrier_lock_test = v19;
GNSS_tracking.var1 = v20;
GNSS_tracking.var2 = v21;
GNSS_tracking.PRN = v22;
end

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src/utils/matlab/libs/plotKalman.m Normal file
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function plotKalman(channelList, trackResults, settings)
% This function plots the tracking results for the given channel list.
%
% plotTracking(channelList, trackResults, settings)
%
% Inputs:
% channelList - list of channels to be plotted.
% trackResults - tracking results from the tracking function.
% settings - receiver settings.
%--------------------------------------------------------------------------
% SoftGNSS v3.0
%
% Copyright (C) Darius Plausinaitis
% Written by Darius Plausinaitis
%--------------------------------------------------------------------------
%This program is free software; you can redistribute it and/or
%modify it under the terms of the GNU General Public License
%as published by the Free Software Foundation; either version 2
%of the License, or (at your option) any later version.
%
%This program is distributed in the hope that it will be useful,
%but WITHOUT ANY WARRANTY; without even the implied warranty of
%MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
%GNU General Public License for more details.
%
%You should have received a copy of the GNU General Public License
%along with this program; if not, write to the Free Software
%Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301,
%USA.
%--------------------------------------------------------------------------
% Protection - if the list contains incorrect channel numbers
channelList = intersect(channelList, 1:settings.numberOfChannels);
%=== For all listed channels ==============================================
for channelNr = channelList
%% Select (or create) and clear the figure ================================
% The number 200 is added just for more convenient handling of the open
% figure windows, when many figures are closed and reopened.
% Figures drawn or opened by the user, will not be "overwritten" by
% this function.
figure(channelNr +200);
clf(channelNr +200);
set(channelNr +200, 'Name', ['Channel ', num2str(channelNr), ...
' (PRN ', ...
num2str(trackResults(channelNr).PRN(end-1)), ...
') results']);
timeStart = settings.timeStartInSeconds;
%% Draw axes ==============================================================
% Row 1
handles(1, 1) = subplot(4, 2, 1);
handles(1, 2) = subplot(4, 2, 2);
% Row 2
handles(2, 1) = subplot(4, 2, 3);
handles(2, 2) = subplot(4, 2, 4);
% Row 3
handles(3, 1) = subplot(4, 2, [5 6]);
% Row 4
handles(4, 1) = subplot(4, 2, [7 8]);
%% Plot all figures =======================================================
timeAxisInSeconds = (1:settings.msToProcess)/1000;
%----- CNo for signal----------------------------------
plot (handles(1, 1), timeAxisInSeconds, ...
trackResults(channelNr).CNo(1:settings.msToProcess), 'b');
grid (handles(1, 1));
axis (handles(1, 1), 'tight');
xlabel(handles(1, 1), 'Time (s)');
ylabel(handles(1, 1), 'CNo (dB-Hz)');
title (handles(1, 1), 'Carrier to Noise Ratio');
%----- PLL discriminator filtered----------------------------------
plot (handles(1, 2), timeAxisInSeconds, ...
trackResults(channelNr).state1(1:settings.msToProcess), 'b');
grid (handles(1, 2));
axis (handles(1, 2), 'tight');
xlim (handles(1, 2), [timeStart, timeAxisInSeconds(end)]);
xlabel(handles(1, 2), 'Time (s)');
ylabel(handles(1, 2), 'Phase Amplitude');
title (handles(1, 2), 'Filtered Carrier Phase');
%----- Carrier Frequency --------------------------------
plot (handles(2, 1), timeAxisInSeconds(2:end), ...
trackResults(channelNr).state2(2:settings.msToProcess), 'Color',[0.42 0.25 0.39]);
grid (handles(2, 1));
axis (handles(2, 1));
xlim (handles(2, 1), [timeStart, timeAxisInSeconds(end)]);
xlabel(handles(2, 1), 'Time (s)');
ylabel(handles(2, 1), 'Freq (hz)');
title (handles(2, 1), 'Filtered Doppler Frequency');
%----- Carrier Frequency Rate --------------------------------
plot (handles(2, 2), timeAxisInSeconds(2:end), ...
trackResults(channelNr).state3(2:settings.msToProcess), 'Color',[0.42 0.25 0.39]);
grid (handles(2, 2));
axis (handles(2, 2));
xlim (handles(2, 2), [timeStart, timeAxisInSeconds(end)]);
xlabel(handles(2, 2), 'Time (s)');
ylabel(handles(2, 2), 'Freq (hz)');
title (handles(2, 2), 'Filtered Doppler Frequency Rate');
%----- PLL discriminator unfiltered--------------------------------
plot (handles(3, 1), timeAxisInSeconds, ...
trackResults(channelNr).innovation, 'r');
grid (handles(3, 1));
axis (handles(3, 1), 'auto');
xlim (handles(3, 1), [timeStart, timeAxisInSeconds(end)]);
xlabel(handles(3, 1), 'Time (s)');
ylabel(handles(3, 1), 'Amplitude');
title (handles(3, 1), 'Raw PLL discriminator (Innovation)');
%----- PLL discriminator covariance --------------------------------
plot (handles(4, 1), timeAxisInSeconds, ...
trackResults(channelNr).r_noise_cov, 'r');
grid (handles(4, 1));
axis (handles(4, 1), 'auto');
xlim (handles(4, 1), [timeStart, timeAxisInSeconds(end)]);
xlabel(handles(4, 1), 'Time (s)');
ylabel(handles(4, 1), 'Variance');
title (handles(4, 1), 'Estimated Noise Variance');
end % for channelNr = channelList