/*! * \file glonass_gnav_almanac.h * \brief Interface of a GLONASS GNAV ALMANAC storage * \note Code added as part of GSoC 2017 program * \author Damian Miralles, 2017. dmiralles2009(at)gmail.com * \see GLONASS ICD * * ----------------------------------------------------------------------------- * * GNSS-SDR is a Global Navigation Satellite System software-defined receiver. * This file is part of GNSS-SDR. * * Copyright (C) 2010-2020 (see AUTHORS file for a list of contributors) * SPDX-License-Identifier: GPL-3.0-or-later * * ----------------------------------------------------------------------------- */ #ifndef GNSS_SDR_GLONASS_ALMANAC_H #define GNSS_SDR_GLONASS_ALMANAC_H #include #include /** \addtogroup Core * \{ */ /** \addtogroup System_Parameters * \{ */ /*! * \brief This class is a storage for the GLONASS SV ALMANAC data as described GLONASS ICD (Edition 5.1) * \note Code added as part of GSoC 2017 program * \see GLONASS ICD */ class Glonass_Gnav_Almanac { public: /*! * Default constructor */ Glonass_Gnav_Almanac() = default; double d_n_A{}; //!< Conventional number of satellite within GLONASS space segment [dimensionless] double d_H_n_A{}; //!< Carrier frequency number of navigation RF signal transmitted by d_nA satellite as table 4.10 (0-31) [dimensionless] double d_lambda_n_A{}; //!< Longitude of the first (within the d_NA day) ascending node of d_nA [radians] double d_t_lambda_n_A{}; //!< Time of first ascending node passage [s] double d_Delta_i_n_A{}; //!< Correction of the mean value of inclination of d_n_A satellite at instant t_lambda_n_A [radians] double d_Delta_T_n_A{}; //!< Correction to the mean value of Draconian period of d_n_A satellite at instant t_lambda_n_A [s / orbital period] double d_Delta_T_n_A_dot{}; //!< Rate of change of Draconian period of d_n_A satellite at instant t_lambda_n_A [s / orbital period^2] double d_epsilon_n_A{}; //!< Eccentricity of d_n_A satellite at instant t_lambda_n_A [dimensionless] double d_omega_n_A{}; //!< Argument of perigee of d_n_A satellite at instant t_lambdan_A [radians] double d_M_n_A{}; //!< Type of satellite n_A [dimensionless] double d_KP{}; //!< Notification on forthcoming leap second correction of UTC [dimensionless] double d_tau_n_A{}; //!< Coarse value of d_n_A satellite time correction to GLONASS time at instant t_lambdan_A[s] bool d_C_n{}; //!< Generalized “unhealthy flag” of n_A satellite at instant of almanac upload [dimensionless] bool d_l_n{}; //!< Health flag for nth satellite; ln = 0 indicates the n-th satellite is helthy, ln = 1 indicates malfunction of this nth satellite [dimensionless] // Satellite Identification Information int32_t i_satellite_freq_channel{}; //!< SV Frequency Channel Number uint32_t PRN{}; //!< SV PRN Number, equivalent to slot number for compatibility with GPS uint32_t i_satellite_slot_number{}; //!< SV Slot Number template /*! * \brief Serialize is a boost standard method to be called by the boost XML * serialization. Here is used to save the almanac data on disk file. */ void serialize(Archive& archive, const uint32_t version) { if (version) { }; archive& BOOST_SERIALIZATION_NVP(i_satellite_freq_channel); archive& BOOST_SERIALIZATION_NVP(PRN); archive& BOOST_SERIALIZATION_NVP(i_satellite_slot_number); archive& BOOST_SERIALIZATION_NVP(d_n_A); archive& BOOST_SERIALIZATION_NVP(d_H_n_A); archive& BOOST_SERIALIZATION_NVP(d_lambda_n_A); archive& BOOST_SERIALIZATION_NVP(d_t_lambda_n_A); archive& BOOST_SERIALIZATION_NVP(d_Delta_i_n_A); archive& BOOST_SERIALIZATION_NVP(d_Delta_T_n_A); archive& BOOST_SERIALIZATION_NVP(d_Delta_T_n_A_dot); archive& BOOST_SERIALIZATION_NVP(d_epsilon_n_A); archive& BOOST_SERIALIZATION_NVP(d_omega_n_A); archive& BOOST_SERIALIZATION_NVP(d_M_n_A); archive& BOOST_SERIALIZATION_NVP(d_KP); archive& BOOST_SERIALIZATION_NVP(d_tau_n_A); archive& BOOST_SERIALIZATION_NVP(d_C_n); archive& BOOST_SERIALIZATION_NVP(d_l_n); } }; /** \} */ /** \} */ #endif // GNSS_SDR_GLONASS_ALMANAC_H