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![Javier Arribas](/assets/img/avatar_default.png)
- The executable file and the default configuration file is now changed from "./install/mercurio" and "./conf/mercurio.conf" to "./install/gnss-sdr" and "./conf/gnss-sdr.conf", respectively. - Configuration file structure changed to define in a single entry the internal sampling frequency (after the signal conditioner). NOTICE that this change affects the all the adapters (acquisition, tracking, telemetry_decoder, observables, and PVT). All the adapters are now modified to work with this feature. - Moved several in-line GPS L1 CA parameters (a.k.a magic numbers..) to ./src/core/system_parameters/GPS_L1_CA.h definition file. - Tracking blocks now uses DOUBLE values in their outputs. - Observables and PVT now are separated. PVT and their associated libraries are moved to ./src/algorithms/PVT - Temporarily disabled the RINEX output (I am working on that!) - GNSS-SDR screen output now gives extended debug information of the receiver status and events. In the future, this output will be redirected to a log file. - Bug fixes: - FILE_SIGNAL_SOURCE now works correctly when the user configures GNSS-SDR to process the entire file. - GPS_L1_CA_DLL_PLL now computes correctly the PRN start values. - GPS_L1_CA_DLL_FLL_PLL now computes correctly the PRN start values. - Several modifications in GPS_L1_CA_Telemetry_Decoder, GPS_L1_CA_Observables, and GPS_L1_CA_PVT modules to fix the GPS position computation. - New features - Tracking blocks perform a signal integrity check against NaN outliers before the correlation process. - Tracking and PVT binary dump options are now documented and we provide MATLAB libraries and sample files to read it. Available in ./utils/matlab" and "./utils/matlab/libs" - Observables output rate can be configured. This option enables the GPS L1 CA PVT computation at a maximum rate of 1ms. - GPS_L1_CA_PVT now can perform a moving average Latitude, Longitude, and Altitude output for each of the Observables output. It is configurable using the configuration file. - Added Google Earth compatible Keyhole Markup Language (KML) output writer class (./src/algorithms/PVT/libs/kml_printer.h and ./src/algorithms/PVT/libs/kml_printer.cc ). You can see the receiver position directly using Google Earth. - We provide a master configuration file which includes an in-line documentation with all the new (and old) options. It can be found in ./conf/master.conf git-svn-id: https://svn.code.sf.net/p/gnss-sdr/code/trunk@84 64b25241-fba3-4117-9849-534c7e92360d
81 lines
2.8 KiB
C++
81 lines
2.8 KiB
C++
/*!
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* \file tracking_2nd_PLL_filter.cc
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* \brief Class that implements 2 order PLL filter for tracking carrier loop.
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* \author Javier Arribas, 2011. jarribas(at)cttc.es
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*
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* Class that implements 2 order PLL filter for tracking carrier loop. The algorithm is described in [1]
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*
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* [1] K.Borre, D.M.Akos, N.Bertelsen, P.Rinder, and S.~H.~Jensen, A Software-Defined GPS and Galileo Receiver. A Single-Frequency Approach,
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* Birkhauser, 2007, Applied and Numerical Harmonic Analysis.
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*
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* -------------------------------------------------------------------------
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*
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* Copyright (C) 2010-2011 (see AUTHORS file for a list of contributors)
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*
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* GNSS-SDR is a software defined Global Navigation
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* Satellite Systems receiver
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*
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* This file is part of GNSS-SDR.
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*
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* GNSS-SDR is free software: you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation, either version 3 of the License, or
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* at your option) any later version.
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*
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* GNSS-SDR is distributed in the hope that it will be useful,
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* but WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with GNSS-SDR. If not, see <http://www.gnu.org/licenses/>.
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*
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* -------------------------------------------------------------------------
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*/
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#include "tracking_2nd_PLL_filter.h"
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void tracking_2nd_PLL_filter::calculate_lopp_coef(float* tau1,float* tau2, float lbw, float zeta, float k){
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// Solve natural frequency
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float Wn;
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Wn = lbw*8*zeta / (4*zeta*zeta + 1);
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// solve for t1 & t2
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*tau1 = k / (Wn * Wn);
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*tau2 = (2.0 * zeta) / Wn;
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}
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void tracking_2nd_PLL_filter::set_PLL_BW(float pll_bw_hz)
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{
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//Calculate filter coefficient values
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d_pllnoisebandwidth=pll_bw_hz;
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calculate_lopp_coef(&d_tau1_carr, &d_tau2_carr, d_pllnoisebandwidth, d_plldampingratio,0.25);// Calculate filter coefficient values
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}
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void tracking_2nd_PLL_filter::initialize(float d_acq_carrier_doppler_hz)
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{
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// carrier/Costas loop parameters
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d_old_carr_nco = 0.0;
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d_old_carr_error = 0.0;
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}
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float tracking_2nd_PLL_filter::get_carrier_nco(float PLL_discriminator)
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{
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float carr_nco;
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carr_nco = d_old_carr_nco+(d_tau2_carr/d_tau1_carr)*(PLL_discriminator - d_old_carr_error) + PLL_discriminator * (d_pdi_carr/d_tau1_carr);
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d_old_carr_nco = carr_nco;
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d_old_carr_error = PLL_discriminator;
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return carr_nco;
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}
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tracking_2nd_PLL_filter::tracking_2nd_PLL_filter ()
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{
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//--- PLL variables --------------------------------------------------------
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d_pdi_carr = 0.001;// Summation interval for carrier
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d_plldampingratio=0.65;
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}
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tracking_2nd_PLL_filter::~tracking_2nd_PLL_filter ()
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{
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}
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