1
0
mirror of https://github.com/gnss-sdr/gnss-sdr synced 2024-11-17 07:14:55 +00:00
gnss-sdr/src/utils/front-end-cal/front_end_cal.h

142 lines
5.4 KiB
C
Raw Normal View History

/*!
* \file front_end_cal.h
* \brief Interface of the Front-end calibration program.
* \author Javier Arribas, 2013. jarribas(at)cttc.es
*
*
* -------------------------------------------------------------------------
*
2015-01-08 18:49:59 +00:00
* Copyright (C) 2010-2015 (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
2015-01-08 18:49:59 +00:00
* (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_FRONT_END_CAL_H_
#define GNSS_SDR_FRONT_END_CAL_H_
#include <armadillo>
#include "file_configuration.h"
#include "concurrent_map.h"
class FrontEndCal
{
private:
std::shared_ptr<ConfigurationInterface> configuration_;
/*!
* \brief LLA2ECEF Convert geodetic coordinates to Earth-centered Earth-fixed
* (ECEF) coordinates. P = LLA2ECEF( LLA ) converts an M-by-3 array of geodetic coordinates
* (latitude, longitude and altitude), LLA, to an M-by-3 array of ECEF
* coordinates, P. LLA is in [degrees degrees meters]. P is in meters.
* The default ellipsoid planet is WGS84. Original copyright (c) by Kai Borre.
*/
arma::vec lla2ecef(arma::vec lla);
/*!
* GEODETIC2ECEF Convert geodetic to geocentric (ECEF) coordinates
* [X, Y, Z] = GEODETIC2ECEF(PHI, LAMBDA, H, ELLIPSOID) converts geodetic
* point locations specified by the coordinate arrays PHI (geodetic
* latitude in radians), LAMBDA (longitude in radians), and H (ellipsoidal
* height) to geocentric Cartesian coordinates X, Y, and Z. The geodetic
* coordinates refer to the reference ellipsoid specified by ELLIPSOID (a
* row vector with the form [semimajor axis, eccentricity]). H must use
* the same units as the semimajor axis; X, Y, and Z will be expressed in
* these units also.
*
* The geocentric Cartesian coordinate system is fixed with respect to the
* Earth, with its origin at the center of the ellipsoid and its X-, Y-,
* and Z-axes intersecting the surface at the following points:
* PHI LAMBDA
* X-axis: 0 0 (Equator at the Prime Meridian)
* Y-axis: 0 pi/2 (Equator at 90-degrees East
* Z-axis: pi/2 0 (North Pole)
*
* A common synonym is Earth-Centered, Earth-Fixed coordinates, or ECEF.
*
* See also ECEF2GEODETIC, ECEF2LV, GEODETIC2GEOCENTRICLAT, LV2ECEF.
*
* Copyright 2004-2009 The MathWorks, Inc.
* $Revision: 1.1.6.4 $ $Date: 2009/04/15 23:34:46 $
* Reference
* ---------
* Paul R. Wolf and Bon A. Dewitt, "Elements of Photogrammetry with
* Applications in GIS," 3rd Ed., McGraw-Hill, 2000 (Appendix F-3).
*/
arma::vec geodetic2ecef(double phi, double lambda, double h, arma::vec ellipsoid);
/*!
* \brief Reads the ephemeris data from an external XML file
*
*/
bool read_assistance_from_XML();
/*!
* \brief Connects to Secure User Location Protocol (SUPL) server to obtain
* the current GPS ephemeris and GPS assistance data.
*
*/
int Get_SUPL_Assist();
const std::string eph_default_xml_filename = "./gps_ephemeris.xml";
public:
/*!
* \brief Sets the configuration data required by get_ephemeris function
*
*/
void set_configuration(std::shared_ptr<ConfigurationInterface> configuration);
/*!
* \brief This function connects to a Secure User Location Protocol (SUPL) server to obtain
* the current GPS ephemeris and GPS assistance data. It requires the configuration parameters set by
* set_configuration function.
*
*/
bool get_ephemeris();
/*!
* \brief This function estimates the GPS L1 satellite Doppler frequency [Hz] using the following data:
* 1- Orbital model from the ephemeris
* 2- Approximate GPS Time of Week (TOW)
* 3- Approximate receiver Latitude and Longitude (WGS-84)
*
*/
double estimate_doppler_from_eph(unsigned int PRN, double TOW, double lat, double lon, double height);
/*!
* \brief This function models the Elonics E4000 + RTL2832 front-end
* Inputs:
* f_bb_true_Hz - Ideal output frequency in baseband [Hz]
* f_in_bb_meas_Hz - measured output frequency in baseband [Hz]
* Outputs:
* estimated_fs_Hz - Sampling frequency estimation based on the
* measurements and the front-end model
* estimated_f_if_bb_Hz - Equivalent bb if frequency estimation based on the
* measurements and the front-end model
* Front-end TUNER Elonics E4000 + RTL2832 sampler For GPS L1 1575.42 MHz
*
*/
void GPS_L1_front_end_model_E4000(double f_bb_true_Hz,double f_bb_meas_Hz,double fs_nominal_hz, double *estimated_fs_Hz, double *estimated_f_if_Hz, double *f_osc_err_ppm );
FrontEndCal();
~FrontEndCal();
};
#endif