/*! * \file Galileo_Navigation_Message.cc * \brief Implementation of a Galileo NAV Data message decoder as described in Galileo ICD * \author Mara Branzanti 2013. mara.branzanti(at)gmail.com * \author Javier Arribas, 2013. jarribas(at)cttc.es * * ------------------------------------------------------------------------- * * Copyright (C) 2010-2013 (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 . * * ------------------------------------------------------------------------- */ #include "galileo_navigation_message.h" #include #include // for boost::crc_basic, boost::crc_optimal #include #include #include #include using namespace std; typedef boost::crc_optimal<24, 0x1864CFBu, 0x0, 0x0, false, false> CRC_Galileo_INAV_type; void Galileo_Navigation_Message::reset() { flag_even_word = 0; /*Word type 1: Ephemeris (1/4)*/ IOD_nav_1 = 0; t0e_1 = 0; M0_1 = 0; e_1 = 0; A_1 = 0; /*Word type 2: Ephemeris (2/4)*/ IOD_nav_2 = 0; // IOD_nav page 2 OMEGA_0_2 = 0; // Longitude of ascending node of orbital plane at weekly epoch [semi-circles] i_0_2 = 0; // Inclination angle at reference time [semi-circles] omega_2 = 0; // Argument of perigee [semi-circles] iDot_2 = 0; // Rate of inclination angle [semi-circles/sec] /*Word type 3: Ephemeris (3/4) and SISA*/ IOD_nav_3 = 0; // OMEGA_dot_3 = 0; // Rate of right ascension [semi-circles/sec] delta_n_3 = 0; // Mean motion difference from computed value [semi-circles/sec] C_uc_3 = 0; // Amplitude of the cosine harmonic correction term to the argument of latitude [radians] C_us_3 = 0; // Amplitude of the sine harmonic correction term to the argument of latitude [radians] C_rc_3 = 0; // Amplitude of the cosine harmonic correction term to the orbit radius [meters] C_rs_3 = 0; // Amplitude of the sine harmonic correction term to the orbit radius [meters] SISA_3 = 0; // /*Word type 4: Ephemeris (4/4) and Clock correction parameters*/ IOD_nav_4 = 0; // SV_ID_PRN_4 = 0; // C_ic_4 = 0; // Amplitude of the cosine harmonic correction term to the angle of inclination [radians] C_is_4 = 0; // Amplitude of the sine harmonic correction term to the angle of inclination [radians] /*Clock correction parameters*/ t0c_4 = 0; // af0_4 = 0; // af1_4 = 0; // af2_4 = 0; // spare_4 = 0; /*Word type 5: Ionospheric correction, BGD, signal health and data validity status and GST*/ /*Ionospheric correction*/ /*Az*/ ai0_5 = 0; // ai1_5 = 0; // ai2_5 = 0; // /*Ionospheric disturbance flag*/ Region1_flag_5 = 0; //Region1_flag_5; Region2_flag_5 = 0; // Region3_flag_5 = 0; // Region4_flag_5 = 0; // Region5_flag_5 = 0; // BGD_E1E5a_5 = 0; // BGD_E1E5b_5 = 0; // E5b_HS_5 = 0; // E1B_HS_5 = 0; // E5b_DVS_5 = 0; // E1B_DVS_5 = 0; // /*GST*/ WN_5 = 0; TOW_5 = 0; spare_5 = 0; /*Word type 6: GST-UTC conversion parameters*/ A0_6 = 0; A1_6 = 0; Delta_tLS_6 = 0; t0t_6 = 0; WNot_6 = 0; WN_LSF_6 = 0; DN_6 = 0; Delta_tLSF_6 = 0; TOW_6 = 0; /*Word type 7: Almanac for SVID1 (1/2), almanac reference time and almanac reference week number*/ IOD_a_7 = 0; WN_a_7 = 0; t0a_7 = 0; SVID1_7 = 0; Delta_alpha_7 = 0; e_7 = 0; omega_7 = 0; delta_i_7 = 0; Omega0_7 = 0; Omega_dot_7 = 0; M0_7 = 0; /*Word type 8: Almanac for SVID1 (2/2) and SVID2 (1/2)*/ IOD_a_8 = 0; af0_8 = 0; af1_8 = 0; E5b_HS_8 = 0; E1B_HS_8 = 0; SVID2_8 = 0; DELTA_A_8 = 0; e_8 = 0; omega_8 = 0; delta_i_8 = 0; Omega0_8 = 0; Omega_dot_8 = 0; /*Word type 9: Almanac for SVID2 (2/2) and SVID3 (1/2)*/ IOD_a_9 = 0; WN_a_9 = 0; t0a_9 = 0; M0_9 = 0; af0_9 = 0; af1_9 = 0; E5b_HS_9 = 0; E1B_HS_9 = 0; SVID3_9 = 0; DELTA_A_9 = 0; e_9 = 0; omega_9 = 0; delta_i_9 = 0; /*Word type 10: Almanac for SVID3 (2/2) and GST-GPS conversion parameters*/ IOD_a_10 = 0; Omega0_10 = 0; Omega_dot_10 = 0; M0_10 = 0; af0_10 = 0; af1_10 = 0; E5b_HS_10 = 0; E1B_HS_10 = 0; A_0G_10 = 0; A_1G_10 = 0; t_0G_10 = 0; WN_0G_10 = 0; /*Word type 0: I/NAV Spare Word*/ Time_0 = 0; WN_0 = 0; TOW_0 = 0; } Galileo_Navigation_Message::Galileo_Navigation_Message() { reset(); } bool Galileo_Navigation_Message::CRC_test(std::bitset bits,boost::uint32_t checksum) { CRC_Galileo_INAV_type CRC_Galileo; boost::uint32_t crc_computed; // Galileo INAV frame for CRC is not an integer multiple of bytes // it needs to be filled with zeroes at the start of the frame. // This operation is done in the transformation from bits to bytes // using boost::dynamic_bitset. // ToDo: Use boost::dynamic_bitset for all the bitset operations in this class boost::dynamic_bitset frame_bits(std::string(bits.to_string())); std::vector bytes; boost::to_block_range(frame_bits, std::back_inserter(bytes)); std::reverse(bytes.begin(),bytes.end()); CRC_Galileo.process_bytes( bytes.data(), GALILEO_DATA_FRAME_BYTES ); crc_computed=CRC_Galileo.checksum(); if (checksum==crc_computed){ return true; }else{ return false; } } unsigned long int Galileo_Navigation_Message::read_navigation_unsigned(std::bitset bits, const std::vector > parameter) { unsigned long int value = 0; int num_of_slices = parameter.size(); for (int i=0; i bits, const std::vector > parameter) { unsigned long int value = 0; int num_of_slices = parameter.size(); for (int i=0; i bits, const std::vector > parameter) { signed long int value = 0; int num_of_slices = parameter.size(); // Discriminate between 64 bits and 32 bits compiler int long_int_size_bytes = sizeof(signed long int); if (long_int_size_bytes == 8) // if a long int takes 8 bytes, we are in a 64 bits system { // read the MSB and perform the sign extension if (bits[GALILEO_DATA_JK_BITS - parameter[0].first] == 1) { value ^= 0xFFFFFFFFFFFFFFFF; //64 bits variable } else { value &= 0; } for (int i=0; i bits, const std::vector > parameter) { bool value; if (bits[GALILEO_DATA_JK_BITS - parameter[0].first] == 1) { value = true; } else { value = false; } return value; } /*void Galileo_Navigation_Message::print_galileo_word_bytes(unsigned int GPS_word) { std::cout << " Word ="; std::cout << std::bitset<32>(GPS_word); std::cout << std::endl; }*/ void Galileo_Navigation_Message::split_page(const char *page, int flag_even_word){ // ToDo: Replace all the C structures and string operations with std::string and std::stringstream C++ classes. // ToDo: Clean all the tests and create an independent google test code for the telemetry decoder. cout << "--------------------------------------------------------------------------" << endl; cout << "Entered in Galileo_Navigation_Message::split_page(char *page)" << endl << endl;; char Even_bit[2]={'\0'}, Odd_bit[2]={'\0'}, Page_type_Odd[2]={'\0'}, Page_type_even[2]={'\0'}, tail_Even[7]={'\0'}; //HO DATO A TUTTI UNO SPAZIO IN PIÙ PER L'ULTIMO CARATTERE char page_Odd[121]={'\0'}; char page_INAV[235]={'\0'}; char Data_j[16]={'\0'}, Data_k[112]={'\0'}, page_number_bits[6]={'\0'}; char Data_jk_ephemeris[129]={'\0'}; char Reserved_1[40]={'\0'}; char SAR[22]={'\0'}; char Spare[2]={'\0'}; char CRC_data[24]={'\0'}; char Reserved_2[8]={'\0'}; char Tail_odd[6]={'\0'}; //char correct_tail[7]="000000"; char correct_tail[7]="011110"; //the viterbi decoder output change the tail to this value (why?) int Page_type=0; static char page_Even[114]; /* Test to decode page 1 even joined to its corresponding The Even pages given here are without their tails bits*/ //test to detect page 1------> char page_Even[115]="000000010001011111010111101101100111110110101110101111100011001000000000001101110101110010000100101010100000010011"; //test to detect page 2------> char page_Even[115]="000000100001011111110010111010111100000010111100000010011100000000100001011110100111000111100111000000100000000010"; //test to detect page 3------>char page_Even[115]="000000110001011111111111111100001001100110001000110001011111110011111100110001011000111110000011011111000011110000"; //test to detect page 4------>char page_Even[115]="000001000001011111001100000000000000101100000000000111010101111011011000000001000101001111101010011100000000010110:// /*test to detect page 5------>char page_Even[115]="000001010010000010000000100010000010111010100000011111110001111111000111111001011000110010110011111111110110000000";*/ //test to detect page 10-----> char page_Even[115]="000010101111101010101010101010101010101010101010101010101010101010101010101010101010111100000000000000000000000000"; //test to detect page 6------>char page_Even[115]="000001100000000000000000000000011100001100000000000000000000000000100011010111111010001101000011100001000110101101 /* test to detect page 7------> char page_Even[115]="000001111111101001011111010011000000000110100000001110010111111110010111110111101001000001110000111111110000101101"; */ /* test to detect page 8------> char page_Even[115]="000010001111000000100001111100000011000001111010100000000000110100000001111010011110111000011110111101001000001110"; */ /* test to detect page 9------> char page_Even[115]="000010011111101001011111111000101110001100000000011010100000000010111111100000001010101010101010101010101010101010"; */ /* test to detect page 10------> char page_Even[115]="000010101111101010101010101010101010101010101010101010101010101010101010101010101010111100000000000000000000000000"; */ /* test to detect page 0------> char page_Even[115]="000000001001010101010101010101010101010101010101010101010101010101010101010101010101010101010101010010110001100101";*/ cout << "Start decoding Galileo I/NAV " << endl; // cout<<"page input"<> s_page_number; // from stringstream to string std::bitset page_type_bits (s_page_number); // from string to bitset Page_type = (int)read_page_type_unsigned(page_type_bits, type); std::cout << "Page number (first 6 bits of Data k converted to decimal) = " << Page_type << endl; strncpy(Data_jk_ephemeris, &Data_k[0], 112); // Join data_j + data_k = Data_jk_ephemeris; strncat(Data_jk_ephemeris, Data_j, 16); // Data_jk_ephemeris is the input for the function page decoder //std::cout<<"Data j k ephemeris" << endl << Data_jk_ephemeris << endl; page_jk_decoder(Data_jk_ephemeris); // Corresponding to ephemeris_decode.m in matlab code //internal_flag_even_word_arrived=0; } } /*if(page[0]=='1') */ else{ strncpy(page_Even, &page[0], 114); //ora che ha memorizzato page even dovrebbe mantenerla per la prossima volta che entro nella funzione std::cout << "Page even in split page" << std::endl << page_Even << std::endl; strncpy(tail_Even, &page[114], 6); if(strcmp (tail_Even,correct_tail) != 0) std::cout << "Tail even is not correct!" << endl; else std::cout<<"Tail even is correct!"<> str; std::bitset data_jk_bits (str); //std::cout << "Data_jk_bits (bitset) "<< endl << data_jk_bits << endl; page_number = (int)read_navigation_unsigned(data_jk_bits, PAGE_TYPE_bit); std::cout << "Page number = " << page_number << endl; switch (page_number) { case 1: /*Word type 1: Ephemeris (1/4)*/ IOD_nav_1=(int)read_navigation_unsigned(data_jk_bits, IOD_nav_1_bit); std::cout<<"IOD_nav_1= "<< IOD_nav_1 <