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https://github.com/gnss-sdr/gnss-sdr
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69b8ac00dc
- 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
34 lines
1.1 KiB
Matlab
34 lines
1.1 KiB
Matlab
function X_sat_rot = e_r_corr(traveltime, X_sat)
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%E_R_CORR Returns rotated satellite ECEF coordinates due to Earth
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%rotation during signal travel time
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%
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%X_sat_rot = e_r_corr(traveltime, X_sat);
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%
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% Inputs:
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% travelTime - signal travel time
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% X_sat - satellite's ECEF coordinates
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%
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% Outputs:
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% X_sat_rot - rotated satellite's coordinates (ECEF)
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%Written by Kai Borre
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%Copyright (c) by Kai Borre
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%
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% CVS record:
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% $Id: e_r_corr.m,v 1.1.1.1.2.6 2006/08/22 13:45:59 dpl Exp $
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%==========================================================================
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Omegae_dot = 7.292115147e-5; % rad/sec
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%--- Find rotation angle --------------------------------------------------
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omegatau = Omegae_dot * traveltime;
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%--- Make a rotation matrix -----------------------------------------------
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R3 = [ cos(omegatau) sin(omegatau) 0;
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-sin(omegatau) cos(omegatau) 0;
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0 0 1];
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%--- Do the rotation ------------------------------------------------------
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X_sat_rot = R3 * X_sat;
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%%%%%%%% end e_r_corr.m %%%%%%%%%%%%%%%%%%%% |