/*! * \file rtklib_pvt_cc.h * \brief Interface of a Position Velocity and Time computation block * \author Javier Arribas, 2017. 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_RTKLIB_PVT_CC_H #define GNSS_SDR_RTKLIB_PVT_CC_H #include "geojson_printer.h" #include "gps_ephemeris.h" #include "gpx_printer.h" #include "kml_printer.h" #include "nmea_printer.h" #include "pvt_conf.h" #include "rinex_printer.h" #include "rtcm_printer.h" #include "rtklib_solver.h" #include #include #include #include #include #include #include #include #include #include #include class rtklib_pvt_cc; typedef boost::shared_ptr rtklib_pvt_cc_sptr; rtklib_pvt_cc_sptr rtklib_make_pvt_cc(uint32_t n_channels, const Pvt_Conf& conf_, const rtk_t& rtk); /*! * \brief This class implements a block that computes the PVT solution using the RTKLIB integrated library */ class rtklib_pvt_cc : public gr::sync_block { private: friend rtklib_pvt_cc_sptr rtklib_make_pvt_cc(uint32_t nchannels, const Pvt_Conf& conf_, const rtk_t& rtk); void msg_handler_telemetry(pmt::pmt_t msg); bool d_dump; bool d_dump_mat; bool b_rinex_output_enabled; bool b_rinex_header_written; bool b_rinex_header_updated; double d_rinex_version; int32_t d_rinexobs_rate_ms; int32_t d_rinexnav_rate_ms; bool b_rtcm_writing_started; bool b_rtcm_enabled; int32_t d_rtcm_MT1045_rate_ms; //!< Galileo Broadcast Ephemeris int32_t d_rtcm_MT1019_rate_ms; //!< GPS Broadcast Ephemeris (orbits) int32_t d_rtcm_MT1020_rate_ms; //!< GLONASS Broadcast Ephemeris (orbits) int32_t d_rtcm_MT1077_rate_ms; //!< The type 7 Multiple Signal Message format for the USA’s GPS system, popular int32_t d_rtcm_MT1087_rate_ms; //!< GLONASS MSM7. The type 7 Multiple Signal Message format for the Russian GLONASS system int32_t d_rtcm_MT1097_rate_ms; //!< Galileo MSM7. The type 7 Multiple Signal Message format for Europe’s Galileo system int32_t d_rtcm_MSM_rate_ms; int32_t d_last_status_print_seg; //for status printer uint32_t d_nchannels; std::string d_dump_filename; int32_t d_output_rate_ms; int32_t d_display_rate_ms; std::shared_ptr rp; std::shared_ptr d_kml_dump; std::shared_ptr d_gpx_dump; std::shared_ptr d_nmea_printer; std::shared_ptr d_geojson_printer; std::shared_ptr d_rtcm_printer; double d_rx_time; bool d_geojson_output_enabled; bool d_gpx_output_enabled; bool d_kml_output_enabled; bool d_nmea_output_file_enabled; std::shared_ptr d_pvt_solver; std::map gnss_observables_map; bool observables_pairCompare_min(const std::pair& a, const std::pair& b); uint32_t type_of_rx; bool first_fix; key_t sysv_msg_key; int sysv_msqid; typedef struct { long mtype; //required by sys v message double ttff; } ttff_msgbuf; bool send_sys_v_ttff_msg(ttff_msgbuf ttff); std::chrono::time_point start, end; bool save_gnss_synchro_map_xml(const std::string& file_name); //debug helper function bool load_gnss_synchro_map_xml(const std::string& file_name); //debug helper function bool d_xml_storage; std::string xml_base_path; inline std::time_t to_time_t(boost::posix_time::ptime pt) { return (pt - boost::posix_time::ptime(boost::gregorian::date(1970, 1, 1))).total_seconds(); } public: rtklib_pvt_cc(uint32_t nchannels, const Pvt_Conf& conf_, const rtk_t& rtk); /*! * \brief Get latest set of ephemeris from PVT block * */ std::map get_gps_ephemeris_map() const; std::map get_gps_almanac_map() const; std::map get_galileo_ephemeris_map() const; std::map get_galileo_almanac_map() const; /*! * \brief Clear all ephemeris information and the almanacs for GPS and Galileo * */ void clear_ephemeris(); /*! * \brief Get the latest Position WGS84 [deg], Ground Velocity, Course over Ground, and UTC Time, if available */ bool get_latest_PVT(double* longitude_deg, double* latitude_deg, double* height_m, double* ground_speed_kmh, double* course_over_ground_deg, time_t* UTC_time); ~rtklib_pvt_cc(); //!< Default destructor int work(int noutput_items, gr_vector_const_void_star& input_items, gr_vector_void_star& output_items); //!< PVT Signal Processing }; #endif