gnss-sdr/src/utils/matlab/libs/geoFunctions/topocent.m

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- Major changes: - 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
2011-12-07 17:59:34 +00:00
function [Az, El, D] = topocent(X, dx)
%TOPOCENT Transformation of vector dx into topocentric coordinate
% system with origin at X.
% Both parameters are 3 by 1 vectors.
%
%[Az, El, D] = topocent(X, dx);
%
% Inputs:
% X - vector origin corrdinates (in ECEF system [X; Y; Z;])
% dx - vector ([dX; dY; dZ;]).
%
% Outputs:
% D - vector length. Units like units of the input
% Az - azimuth from north positive clockwise, degrees
% El - elevation angle, degrees
%Kai Borre 11-24-96
%Copyright (c) by Kai Borre
%
% CVS record:
% $Id: topocent.m,v 1.1.1.1.2.4 2006/08/22 13:45:59 dpl Exp $
%==========================================================================
dtr = pi/180;
[phi, lambda, h] = togeod(6378137, 298.257223563, X(1), X(2), X(3));
cl = cos(lambda * dtr);
sl = sin(lambda * dtr);
cb = cos(phi * dtr);
sb = sin(phi * dtr);
F = [-sl -sb*cl cb*cl;
cl -sb*sl cb*sl;
0 cb sb];
local_vector = F' * dx;
E = local_vector(1);
N = local_vector(2);
U = local_vector(3);
hor_dis = sqrt(E^2 + N^2);
if hor_dis < 1.e-20
Az = 0;
El = 90;
else
Az = atan2(E, N)/dtr;
El = atan2(U, hor_dis)/dtr;
end
if Az < 0
Az = Az + 360;
end
D = sqrt(dx(1)^2 + dx(2)^2 + dx(3)^2);
%%%%%%%%% end topocent.m %%%%%%%%%