/*!
* \file galileo_navigation_message.h
* \brief Implementation of a Galileo I/NAV Data message
* as described in Galileo OS SIS ICD Issue 1.2 (Nov. 2015)
* \author Mara Branzanti 2013. mara.branzanti(at)gmail.com
* \author Javier Arribas, 2013. 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 .
*
* -------------------------------------------------------------------------
*/
#ifndef GNSS_SDR_GALILEO_NAVIGATION_MESSAGE_H_
#define GNSS_SDR_GALILEO_NAVIGATION_MESSAGE_H_
#include "Galileo_E1.h"
#include "galileo_almanac_helper.h"
#include "galileo_ephemeris.h"
#include "galileo_iono.h"
#include "galileo_utc_model.h"
#include
#include
#include
#include
#include
/*!
* \brief This class handles the Galileo I/NAV Data message, as described in the
* Galileo Open Service Signal in Space Interface Control Document (OS SIS ICD), Issue 1.2 (Nov 2015).
* See https://www.gsc-europa.eu/system/files/galileo_documents/Galileo_OS_SIS_ICD.pdf
*/
class Galileo_Navigation_Message
{
public:
Galileo_Navigation_Message();
int32_t Page_type_time_stamp;
int32_t flag_even_word;
std::string page_Even;
bool flag_CRC_test;
bool flag_all_ephemeris; //!< Flag indicating that all words containing ephemeris have been received
bool flag_ephemeris_1; //!< Flag indicating that ephemeris 1/4 (word 1) have been received
bool flag_ephemeris_2; //!< Flag indicating that ephemeris 2/4 (word 2) have been received
bool flag_ephemeris_3; //!< Flag indicating that ephemeris 3/4 (word 3) have been received
bool flag_ephemeris_4; //!< Flag indicating that ephemeris 4/4 (word 4) have been received
bool flag_iono_and_GST; //!< Flag indicating that ionospheric and GST parameters (word 5) have been received
bool flag_TOW_5;
bool flag_TOW_6;
bool flag_TOW_set; //!< it is true when page 5 or page 6 arrives
bool flag_utc_model; //!< Flag indicating that utc model parameters (word 6) have been received
bool flag_all_almanac; //!< Flag indicating that all almanac have been received
bool flag_almanac_1; //!< Flag indicating that almanac 1/4 (word 7) have been received
bool flag_almanac_2; //!< Flag indicating that almanac 2/4 (word 8) have been received
bool flag_almanac_3; //!< Flag indicating that almanac 3/4 (word 9) have been received
bool flag_almanac_4; //!< Flag indicating that almanac 4/4 (word 10) have been received
int32_t IOD_ephemeris;
bool flag_GGTO;
bool flag_GGTO_1;
bool flag_GGTO_2;
bool flag_GGTO_3;
bool flag_GGTO_4;
// Word type 1: Ephemeris (1/4)
int32_t IOD_nav_1; //!< IOD_nav page 1
int32_t t0e_1; //!< Ephemeris reference time [s]
double M0_1; //!< Mean anomaly at reference time [semi-circles]
double e_1; //!< Eccentricity
double A_1; //!< Square root of the semi-major axis [meters^1/2]
// Word type 2: Ephemeris (2/4)
int32_t IOD_nav_2; //!< IOD_nav page 2
double OMEGA_0_2; //!< Longitude of ascending node of orbital plane at weekly epoch [semi-circles]
double i_0_2; //!< Inclination angle at reference time [semi-circles]
double omega_2; //!< Argument of perigee [semi-circles]
double iDot_2; //!< Rate of inclination angle [semi-circles/sec]
// Word type 3: Ephemeris (3/4) and SISA
int32_t IOD_nav_3; //
double OMEGA_dot_3; //!< Rate of right ascension [semi-circles/sec]
double delta_n_3; //!< Mean motion difference from computed value [semi-circles/sec]
double C_uc_3; //!< Amplitude of the cosine harmonic correction term to the argument of latitude [radians]
double C_us_3; //!< Amplitude of the sine harmonic correction term to the argument of latitude [radians]
double C_rc_3; //!< Amplitude of the cosine harmonic correction term to the orbit radius [meters]
double C_rs_3; //!< Amplitude of the sine harmonic correction term to the orbit radius [meters]
int32_t SISA_3;
// Word type 4: Ephemeris (4/4) and Clock correction parameters*/
int32_t IOD_nav_4; //
int32_t SV_ID_PRN_4; //
double C_ic_4; //! bits, uint32_t checksum);
bool read_navigation_bool(std::bitset bits, const std::vector >& parameter);
uint64_t read_navigation_unsigned(std::bitset bits, const std::vector >& parameter);
uint64_t read_page_type_unsigned(std::bitset bits, const std::vector >& parameter);
int64_t read_navigation_signed(std::bitset bits, const std::vector >& parameter);
};
#endif /* GALILEO_NAVIGATION_MESSAGE_H_ */