/** * @file Satellite based augmentation system (SBAS) * @see DO-229D */ /* * Copyright (c) 2018, M.Naruoka (fenrir) * All rights reserved. * * Redistribution and use in source and binary forms, with or without modification, * are permitted provided that the following conditions are met: * * - Redistributions of source code must retain the above copyright notice, * this list of conditions and the following disclaimer. * - Redistributions in binary form must reproduce the above copyright notice, * this list of conditions and the following disclaimer in the documentation * and/or other materials provided with the distribution. * - Neither the name of the naruoka.org nor the names of its contributors * may be used to endorse or promote products derived from this software * without specific prior written permission. * * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS" * AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, * THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE * ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT HOLDER OR CONTRIBUTORS * BE LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, * OR CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, * PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; * LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) * HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, * STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) * ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, * EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE. * */ #ifndef __SBAS_H__ #define __SBAS_H__ #include #include #include #include #include #include #include "GPS.h" template class SBAS_Signal { public: typedef FloatT float_t; class G2 : public GPS_Signal::PRN { public: typedef typename GPS_Signal::PRN super_t; G2(const int &initial_g2) : super_t((unsigned long)initial_g2) {} ~G2(){} bool get() const {return super_t::_content[9];} void next(){ bool tmp(super_t::_content[1] ^ super_t::_content[2] ^ super_t::_content[5] ^ super_t::_content[7] ^ super_t::_content[8] ^ super_t::_content[9]); super_t::_content <<= 1; super_t::_content[0] = tmp; } }; }; template class SBAS_SpaceNode { public: typedef FloatT float_t; typedef GPS_SpaceNode gps_space_node_t; #define type_copy(type) \ typedef typename gps_space_node_t::type type type_copy(gps_time_t); type_copy(xyz_t); type_copy(enu_t); type_copy(llh_t); type_copy(u8_t); type_copy(s8_t); type_copy(u16_t); type_copy(s16_t); type_copy(u32_t); type_copy(s32_t); type_copy(int_t); type_copy(uint_t); #undef type_copy struct RangingCode { int prn; int g2_delay_chips; int initial_g2; float_t lng_deg; const char *name; typename SBAS_Signal::G2 get_G2() const { return typename SBAS_Signal::G2(initial_g2); } struct prn_sorter_t { bool operator()(const RangingCode *left, const RangingCode *right) const { return (left->prn < right->prn); } }; struct lng_sorter_t { bool operator()(const RangingCode *left, const RangingCode *right) const { return (left->lng_deg < right->lng_deg); } }; struct lng_sorter2_t { float_t base_lng_deg; lng_sorter2_t(const float_t &lng_deg) : base_lng_deg(lng_deg) {} bool operator()(const RangingCode *left, const RangingCode *right) const { float_t delta_l(left->lng_deg - base_lng_deg); if(delta_l < 0){delta_l *= -1;} if(delta_l >= 180){delta_l = -delta_l + 360;} float_t delta_r(right->lng_deg - base_lng_deg); if(delta_r < 0){delta_r *= -1;} if(delta_r >= 180){delta_r = -delta_r + 360;} return (delta_l < delta_r); } }; struct name_sorter_t { bool operator()(const RangingCode *left, const RangingCode *right) const { int cmp(std::strcmp(left->name, right->name)); return cmp != 0 ? (cmp < 0) : (left->prn < right->prn); } }; }; struct KnownSatellites { typedef std::vector list_t; template static list_t sort(T sorter); static const list_t prn_ordered; static const list_t longitude_ordered; static const list_t name_ordered; static list_t nearest_ordered(const float_t &lng_deg){ return sort(typename RangingCode::lng_sorter2_t(lng_deg)); } }; enum MessageType { DONT_USE = 0, PRN_MASK = 1, FAST_CORRECTION_2 = 2, FAST_CORRECTION_3 = 3, FAST_CORRECTION_4 = 4, FAST_CORRECTION_5 = 5, INTEGRITY_INFORMATION = 6, FAST_CORRECTION_DEGRADATION = 7, GEO_NAVIGATION = 9, DEGRADATION_PARAMS = 10, SBAS_NETWORK_TIME_UTC_OFFSET_PARAMS = 12, GEO_SAT_ALNAMACS = 17, IONO_GRID_POINT_MASKS = 18, MIXED_CORRECTION_FAST_AND_LONG_TERM = 24, LONG_TERM_CORRECTION = 25, IONO_DELAY_CORRECTION = 26, SERVICE_MESSAGE = 27, CLOCK_EPHEMERIS_COV_MAT = 28, INTERNAL_TEST_MESSAGE = 62, NULL_MESSAGES = 63, UNSUPPORTED_MESSAGE = 64, }; ///< @see Table A-3 struct Timing { enum { DONT_USE_FOR_SAFETY_APPLICATIONS, PRN_MASK, UDREI, FAST_CORRECTIONS, LONG_TERM_CORRECTIONS, GEO_NAVIGATION_DATA, FAST_CORRECTION_DEGRADATION, DEGRADATION_PARAMETERS, IONOSPHERIC_GRID_MASK, IONOSPHERIC_CORRECTIONS, UTC_TIMING_DATA, ALNAMAC_DATA, SERVICE_LEVEL, CLOCK_EPHEMERIS_COVARIANCE_MATRIX, NUM_OF_TIMING_ITEMS, }; struct values_t { int interval, timeout_EN_Route_Terminal_LNAV, timeout_LNAV_VNAV_LP_LPV_approach; }; static const values_t values[NUM_OF_TIMING_ITEMS]; }; ///< @see Table A-25; struct DataBlock : public gps_space_node_t::DataParser { typedef typename gps_space_node_t::DataParser parser_t; #define convert_u(bits, offset_bits, length, name) \ template \ static u ## bits ## _t name(const InputT *buf){ \ return parser_t::template bits2num( \ buf, offset_bits, length); \ } #define convert_s(bits, offset_bits, length, name) \ template \ static s ## bits ## _t name(const InputT *buf){ \ return (s ## bits ## _t)parser_t::template bits2num( \ buf, offset_bits) \ >> (bits - length); \ } #define convert_u_ch(bits, offset_bits, length, bits_per_ch, name) \ template \ static u ## bits ## _t name(const InputT *buf, const uint_t &ch){ \ return parser_t::template bits2num( \ buf, offset_bits + (bits_per_ch * ch), length); \ } #define convert_s_ch(bits, offset_bits, length, bits_per_ch, name) \ template \ static s ## bits ## _t name(const InputT *buf, const uint_t &ch){ \ return (s ## bits ## _t)parser_t::template bits2num( \ buf, offset_bits + (bits_per_ch * ch)) \ >> (bits - length); \ } /** * Convert bit pattern to indices array having '1' * Ex) 0b00100100 => [2, 5] * @param buf bit pattern * @param indices array to which results are stored * @param length length of bits to be inspected * @param offset starting offset of bits * @return number of '1' */ template static u8_t bits2linear( const InputT *buf, u8_t *indices, const u8_t &length, const u8_t &offset = 0){ u8_t *hits(indices); std::div_t aligned(std::div(offset, (int)sizeof(InputT) * 8)); buf += aligned.quot; InputT compared((InputT)0x1 << (sizeof(InputT) * 8 - aligned.rem - 1)); // [mask7, mask6, .., mask0], [mask15, mask14, .., mask8], ... for(u8_t i(0); i < length; ++i, compared >>= 1){ if(compared == 0){ // rotate compared = ((InputT)0x1 << (sizeof(InputT) * 8 - 1)); buf++; } if(*buf & compared){ *(hits++) = i; } } return hits - indices; } convert_u(8, 0, 8, preamble); convert_u(8, 8, 6, message_type); struct Type1 { ///< @see Fig. A-6 PRN_MASK struct mask_t { u8_t valid; static const int each_block = 13; union { u8_t prn_minus_one[210]; u8_t block[4][each_block]; }; }; template static mask_t mask(const InputT *buf, const u8_t &band){ mask_t res; res.valid = bits2linear(buf, res.prn_minus_one, 210, 14); // 14 bit shift if(res.valid > 51){res.valid = 0;} // invalid, because up to 51 masks return res; } convert_u(8, 224, 2, iodp); }; struct Type2_5 { ///< @see Fig. A-7 FAST_CORRECTION_2-5 convert_u( 8, 14, 2, iodf); convert_u( 8, 16, 2, iodp); convert_s_ch(16, 18, 12, 12, prc_f); // pseudo range correction (fast) convert_u_ch( 8, 174, 4, 4, udrei); }; struct Type6 { ///< @see Fig. A-8, Table A-5 INTEGRITY_INFORMATION convert_u_ch( 8, 14, 2, 2, iodf); // iodf2-5 convert_u_ch( 8, 22, 4, 4, udrei); }; struct Type7 { ///< @see Fig. A-9, Table A-7 FAST_CORRECTION_DEGRADATION convert_u( 8, 14, 4, t_lat); convert_u( 8, 18, 2, iodp); convert_u_ch( 8, 22, 4, 4, ai_i); }; struct Type25 { ///< @see Fig. A-10,11, Table A-10,11 LONG_TERM_CORRECTION convert_u_ch( 8, 14, 1, 106, vel_code); convert_u_ch( 8, 15, 6, 106, prn_mask); convert_u_ch( 8, 21, 8, 106, iod); struct V0 { convert_s_ch(16, 29, 9, 106, dx); convert_s_ch(16, 38, 9, 106, dy); convert_s_ch(16, 47, 9, 106, dz); convert_s_ch(16, 56, 10, 106, da_f0); convert_u_ch( 8, 66, 6, 106, prn_mask_2); convert_u_ch( 8, 72, 8, 106, iod_2); convert_s_ch(16, 80, 9, 106, dx_2); convert_s_ch(16, 89, 9, 106, dy_2); convert_s_ch(16, 98, 9, 106, dz_2); convert_s_ch(16, 107, 10, 106, da_f0_2); convert_u_ch( 8, 117, 2, 106, iodp); }; struct V1 { convert_s_ch(16, 29, 11, 106, dx); convert_s_ch(16, 40, 11, 106, dy); convert_s_ch(16, 51, 11, 106, dz); convert_s_ch(16, 62, 11, 106, da_f0); convert_s_ch( 8, 73, 8, 106, dx_dot); convert_s_ch( 8, 81, 8, 106, dy_dot); convert_s_ch( 8, 89, 8, 106, dz_dot); convert_s_ch( 8, 97, 8, 106, da_f1); convert_u_ch(16, 105, 13, 106, t_0); convert_u_ch( 8, 118, 2, 106, iodp); }; }; struct Type24 : public Type25 { ///< @see Fig. A-12 MIXED_CORRECTION_FAST_AND_LONG_TERM convert_s_ch(16, 14, 12, 12, prc_f); // pseudo range correction (fast) convert_u_ch( 8, 86, 4, 4, udrei); convert_u( 8, 110, 2, iodp); convert_u( 8, 112, 2, block_id); // 1-6(Type2), 14-19(Type3), 27-32(Type4), 40-45(Type5) convert_u( 8, 114, 2, iodf); // Second half of 106 bits are same as Type25(ch1) }; struct Type18 { ///< @see Table A-15 IONO_GRID_POINT_MASKS convert_u(8, 14, 4, broadcasted_bands); convert_u(8, 18, 4, band); convert_u(8, 22, 2, iodi); struct mask_t { u8_t valid; static const int each_block = 15; union { u8_t linear[201]; u8_t block[14][each_block]; }; }; /** * @param band [0,10] * @return Number of mask bits */ static u8_t mask_bits(const u8_t &band){ switch(band){ case 8: return 200; case 9: case 10: return 192; default: return 201; } } template static mask_t mask(const InputT *buf, const u8_t &band){ mask_t res; res.valid = bits2linear(buf, res.linear, mask_bits(band), 24); // 24 bit shift return res; } template static mask_t mask(const InputT *buf){ return mask(buf, band(buf)); } }; struct Type26 { ///< @see Table A-16 IONO_DELAY_CORRECTION convert_u(8, 14, 4, band); convert_u(8, 18, 4, block_id); convert_u_ch(16, 22, 9, 13, delay); convert_u_ch( 8, 31, 4, 13, error_indicator); convert_u(8, 22 + (13 * 15), 2, iodi); // 22 + (13 * 15) + 2 + 7(spare) + 24(parity) = 250 }; struct Type9 { ///< @see Table A-18 GEO_NAVIGATION convert_u(16, 22, 13, t0); convert_u( 8, 35, 4, ura); convert_s(32, 39, 30, x); convert_s(32, 69, 30, y); convert_s(32, 99, 25, z); convert_s(32, 124, 17, dx); convert_s(32, 141, 17, dy); convert_s(32, 158, 18, dz); convert_s(16, 176, 10, ddx); convert_s(16, 186, 10, ddy); convert_s(16, 196, 10, ddz); convert_s(16, 206, 12, a_Gf0); convert_s( 8, 218, 8, a_Gf1); }; struct Type10 { ///< @see Table A-9 Degradation factors convert_u(16, 14, 10, B_rcc); convert_u(16, 24, 10, C_ltc_lsb); convert_u(16, 34, 10, C_ltc_v1); convert_u(16, 44, 9, I_ltc_v1); convert_u(16, 53, 10, C_ltc_v0); convert_u(16, 63, 9, I_ltc_v0); convert_u(16, 72, 10, C_geo_lsb); convert_u(16, 82, 10, C_geo_v); convert_u(16, 92, 9, I_geo); convert_u( 8, 101, 6, C_er); convert_u(16, 107, 10, C_iono_step); convert_u(16, 117, 9, I_iono); convert_u(16, 126, 10, C_iono_ramp); convert_u( 8, 136, 1, RSS_UDRE); convert_u( 8, 137, 1, RSS_iono); convert_u( 8, 138, 7, C_covariance); // 138 + 7 + 81(spare) + 24(parity) = 250 }; struct Type17 { ///< @see Table A-17 GEO_SAT_ALNAMACS convert_u_ch( 8, 14, 2, 67, id); convert_u_ch( 8, 16, 8, 67, prn); convert_u_ch( 8, 24, 8, 67, health_status); convert_s_ch(16, 32, 15, 67, x); convert_s_ch(16, 47, 15, 67, y); convert_s_ch(16, 62, 9, 67, z); convert_s_ch( 8, 71, 3, 67, x_dot); convert_s_ch( 8, 74, 3, 67, y_dot); convert_s_ch( 8, 77, 4, 67, z_dot); convert_u(16, 215, 11, t0); }; struct Type12 { // @see Table A-22 SBAS network Time/UTC parameters convert_s(32, 14, 24, A1_SNT); convert_s(32, 38, 32, A0_SNT); convert_u( 8, 70, 8, t_ot); convert_u( 8, 78, 8, WN_t); convert_s( 8, 86, 8, delta_t_LS); convert_u( 8, 94, 8, WN_LSF); convert_u( 8, 102, 8, DN); convert_s( 8, 110, 8, delta_t_LSF); convert_u( 8, 118, 3, UTC_standard_identifier); convert_u(32, 121, 20, TOW); convert_u(16, 141, 10, WN); }; #undef convert_s_ch #undef convert_u_ch #undef convert_s #undef convert_u }; struct DegradationFactors { float_t B_rcc; float_t C_ltc_lsb; float_t C_ltc_v1; int I_ltc_v1; float_t C_ltc_v0; int I_ltc_v0; float_t C_geo_lsb; float_t C_geo_v; int I_geo; float_t C_er; float_t C_iono_step; int I_iono; float_t C_iono_ramp; bool RSS_UDRE; bool RSS_iono; float_t C_covariance; struct raw_t { enum { SF_B_rcc, SF_C_ltc_lsb, SF_C_ltc_v1, SF_C_ltc_v0, SF_C_geo_lsb, SF_C_geo_v, SF_C_er, SF_C_iono_step, SF_C_iono_ramp, SF_C_covariance, SF_NUM, }; static const float_t sf[SF_NUM]; template static DegradationFactors fetch(const InputT *buf){ typedef typename DataBlock::Type10 msg_t; DegradationFactors res = { #define CONVERT(TARGET) \ sf[SF_ ## TARGET] * msg_t::TARGET(buf) CONVERT(B_rcc), CONVERT(C_ltc_lsb), CONVERT(C_ltc_v1), msg_t::I_ltc_v1(buf), CONVERT(C_ltc_v0), msg_t::I_ltc_v0(buf), CONVERT(C_geo_lsb), CONVERT(C_geo_v), msg_t::I_geo(buf), CONVERT(C_er), CONVERT(C_iono_step), msg_t::I_iono(buf), CONVERT(C_iono_ramp), (msg_t::RSS_UDRE(buf) == 1), (msg_t::RSS_iono(buf) == 1), CONVERT(C_covariance), #undef CONVERT }; return res; } }; }; class IonosphericGridPoints { public: struct PointProperty { float_t delay; // [m] float_t sigma2; // [m^2], negative value means "not monitored" struct raw_t { u16_t delay; u8_t error_indicator; template static raw_t fetch(const InputT *buf, const uint_t &ch){ typedef typename DataBlock::Type26 msg_t; raw_t res = { msg_t::delay(buf, ch), // delay msg_t::error_indicator(buf, ch), // error_indicator }; return res; } enum { DELAY_DONT_USE = 0x1FF, ERROR_INDICATOR_NOT_MONITORED = 15, }; static const raw_t unavailable; static float_t raw2delay(const u16_t &v){ return 0.125 * v; } static float_t raw2sigma2(const u8_t &v){ switch(v){ ///< @see Table A-17 case 0: return 0.0084; case 1: return 0.0333; case 2: return 0.0749; case 3: return 0.1331; case 4: return 0.2079; case 5: return 0.2994; case 6: return 0.4075; case 7: return 0.5322; case 8: return 0.6735; case 9: return 0.8315; case 10: return 1.1974; case 11: return 1.8709; case 12: return 3.3260; case 13: return 20.7870; case 14: return 187.0826; } return -1; } operator PointProperty() const { PointProperty res = { raw2delay(delay), raw2sigma2(error_indicator), }; return res; } bool is_available() const { return (delay < DELAY_DONT_USE) && (error_indicator < ERROR_INDICATOR_NOT_MONITORED); } }; bool is_available() const { return (sigma2 > 0); } static const PointProperty unavailable; }; struct position_index_t; struct position_t { int_t latitude_deg; ///< latitude in degrees, north is positive. [-85, 85]. int_t longitude_deg; ///< longitude in degrees, east is positive. [-180, 175] operator position_index_t() const; bool is_predefined() const { // range check if((latitude_deg < -85) || (latitude_deg > 85)){return false;} if((longitude_deg < -180) || (longitude_deg >= 180)){return false;} // at least, on 5 deg grid if((latitude_deg + 85) % 5 != 0){return false;} int_t lng_reg(longitude_deg + 180); if(lng_reg % 5 != 0){return false;} switch(latitude_deg){ case 80: case -80: return false; case 85: return (lng_reg % 30 == 0); // W180(=0), W150(=30), ... case -85: return (lng_reg % 30 == 10); // W170(=10), W140(=40), ... } if((latitude_deg >= 65) || (latitude_deg <= -65)){ return (lng_reg % 10 == 0); } return true; } /** * Compute longitude difference from another IGP. * @param from * @return difference (always positive) [0, 360) */ int_t delta_lng(const position_t &from) const { int_t res(longitude_deg - from.longitude_deg); return (res < 0) ? (res + 360) : res; } }; /** * Resolve ionospheric grid point position * @param band valid range is [0, 10] * @param mask_pos valid range is [0, 200 (or 199, 191)] (be careful, not [1, 201]) * @return (pos_t) grid point position * @see Table A-14 */ static position_t position(const u8_t &band, const u8_t &mask_pos){ position_t res; if(band <= 8){ u8_t row_index_28(band & (~(u8_t)0x01)); // where 28 grid points on the same longitude are appeared int row_index(0), col_index((int)mask_pos); do{ int points(row_index_28 == row_index ? 28 : 27); if(col_index < points){ col_index -= 2; // col_index => [-2, 24 (or 25)] if((points > 27) && (band % 2 == 1)){ // col_index => [-3, 24] col_index--; } break; } col_index -= points; row_index++; points = 23; if(col_index < points){break;} col_index -= points; row_index++; }while(row_index < 8); if(row_index < 8){ res.longitude_deg = -180 + band * 40 + row_index * 5; switch(col_index){ case -3: res.latitude_deg = -85; break; case -2: res.latitude_deg = -75; break; case -1: res.latitude_deg = -65; break; case 23: res.latitude_deg = 65; break; case 24: res.latitude_deg = 75; break; case 25: res.latitude_deg = 85; break; default: res.latitude_deg = -55 + col_index * 5; break; } } }else if(band <= 10){ if(mask_pos < 72){ res.latitude_deg = 60 * ((band == 10) ? -1 : 1); res.longitude_deg = mask_pos * 5 - 180; }else if(mask_pos < 180){ std::div_t a(std::div(mask_pos - 72, 36)); res.latitude_deg = (65 + a.quot * 5) * ((band == 10) ? -1 : 1); res.longitude_deg = a.rem * 10 - 180; }else if(mask_pos < 192){ res.latitude_deg = 85; res.longitude_deg = (mask_pos - 180) * 30 - 180; if(band == 10){ res.latitude_deg *= -1; res.longitude_deg += 10; if(res.longitude_deg > 180){ res.longitude_deg -= 360; } } } } return res; } struct position_index_t { int_t lat_index; ///< Latitude index; N85(0), N75(1), N70(2), N65(3), N60(4), ..., 0(16) ..., S60(28), S65(29), S70(30), S75(31), S85(32) int_t lng_index; ///< Longitude index; W180(0), W175(1), W170(2), ..., 0(36), ..., E170(70), E175(71) enum { LAT_INDEX_N85 = 0, // 30 deg grid LAT_INDEX_N75 = 1, // 10 deg grid LAT_INDEX_N65 = 3, // 10 deg grid LAT_INDEX_S65 = 29, // 10 deg grid LAT_INDEX_S75 = 31, // 10 deg grid LAT_INDEX_S85 = 32, // 30 deg grid LAT_INDEX_MAX = LAT_INDEX_S85, }; enum { LNG_INDEX_MAX = 71, }; ///< Convert latitude in degrees to index static int_t lat2idx(const int_t &lat_deg){ return (lat_deg == 85) ? LAT_INDEX_N85 : ((lat_deg == -85) ? LAT_INDEX_S85 : (80 - lat_deg) / 5); } ///< Convert latitude index to degrees static int_t idx2lat(const int_t &lat_idx){ return (lat_idx % 32 == 0) ? ((lat_idx == 0) ? 85 : -85) : ((16 - lat_idx) * 5); } ///< Convert longitude in degrees to index static int_t lng2idx(const int_t &lng_deg){ return (lng_deg + 180) / 5; } ///< Convert longitude index to degrees static int_t idx2lng(const int_t &lng_idx){ return (lng_idx - 36) * 5; } operator position_t() const { position_t res = {idx2lat(lat_index), idx2lng(lng_index)}; return res; } }; struct pivot_t { position_t igp; struct { float_t latitude_deg, longitude_deg; } delta; }; /** * Get a pivot IGP, and compute distance (delta) from the IGP. * The "pivot" one means "nearest west, and north if in south hemisphere, * south if otherwise (in north hemisphere, or on equator), one". * If the specified input latitude is not identical to zero, and exactly same as a latitude where IGPs exist, * then the return IGP is shifted to the nearest west (north hemisphere) or north (east hemisphere) point. * For example: * 1) (lat, lng) = (10, 0) => igp = {5, 0}, delta = {5, 0} * 2) (lat, lng) = (85, 15) => igp = {75, 10}, delta = {10, 5} * @param latitude_deg latitude in degrees; [-90, 90] * @param longitude_deg longitude in degrees * @return pivot IGP position and delta */ template static pivot_t get_pivot(const T &latitude_deg, const T &longitude_deg){ T lng(longitude_deg); // => [-180, 180) int_t lng_reg; // => [0, 360), mapping W180(=> 0), ... E180(=> 360) { if(longitude_deg < -180){ lng += (((int_t)(-longitude_deg + 180) / 360) * 360); // => [-*, -180) => (-180, 180] if(lng == 180){ lng -= 360; // 180 => -180 } }else{ lng -= (((int_t)(longitude_deg + 180) / 360) * 360); // => [-180, +*] => [-180, 180) } lng_reg = 180 + lng; // => [0, 360) } pivot_t res; if(latitude_deg > 85){ res.igp.latitude_deg = 85; lng_reg = (lng_reg / 90) * 90; // W180, W90, ... @see A 4.4.10.2 d), and P-2 /*if(latitude_deg == 85){ // intentionally commented out; when exactly same as lat == 85, // a lat-10 deg grid will be used, because of P-2. lng_reg = (lng_reg / 30) * 30; // W180, W150, ... }*/ }else if(latitude_deg < -85){ res.igp.latitude_deg = -85; lng_reg = (lng_reg < 40) ? (130 + 180) : (((lng_reg - 40) / 90) * 90 + 40); // W140, W50, ... @see A 4.4.10.2 e), and P-2 /*if(latitude_deg == -85){ // intentionally commented out lng_reg = (lng_reg < 10) ? (160 + 180) : (((lng_reg - 10) / 30) * 30 + 10); // W170, W140, ... }*/ }else{ if(latitude_deg > 75){ res.igp.latitude_deg = 75; }else if(latitude_deg < -75){ res.igp.latitude_deg = -75; }else{ if(latitude_deg >= 0){ res.igp.latitude_deg = ((int_t)latitude_deg / 5) * 5; }else{ res.igp.latitude_deg = -((int_t)(-latitude_deg) / 5) * 5; } if((res.igp.latitude_deg == latitude_deg) && (res.igp.latitude_deg != 0)){ // on grid point latitude, see P-2 res.igp.latitude_deg += (res.igp.latitude_deg > 0 ? -5 : 5); } } if((res.igp.latitude_deg >= 60) || (res.igp.latitude_deg <= -60)){ lng_reg = (lng_reg / 10) * 10; // W180, W170, ... }else{ lng_reg = (lng_reg / 5) * 5; // W180, W175, ... } } res.igp.longitude_deg = lng_reg - 180; // [0, 360) => [-180, 180) res.delta.latitude_deg = latitude_deg - res.igp.latitude_deg; res.delta.longitude_deg = lng - res.igp.longitude_deg; if(res.delta.longitude_deg < 0){res.delta.longitude_deg += 360;} // always east (delta.lng >= 0) return res; } struct trapezoid_t { /** * igp(2)=[1] -- igp(1)=[0] igp(3)=[2] -- igp(4)=[3] * | | in north, | | in south * igp(3)=[2] -- igp(4)=[3] igp(2)=[1] -- igp(1)=[0] * This is based on Fig.A-19. * result of get_pivot() will be assigned to igp(3)=[2]. * * assumption * igp[0].lat = igp[1].lat, igp[2].lat = igp[3].lat * igp[1].lng < igp[0].lng, igp[2].lng < igp[3].lng, (igp[1].lng is not necessarily indentical to igp[2].lng) */ position_t igp[4]; bool checked[4]; ///< If igp[i] has been check to be available, true; otherwise, false. float_t weight[4]; /** * @param delta_phi * @param delta_lambda * @see Fig.A-19 */ void compute_weight(const float_t &delta_phi, const float_t &delta_lambda){ // (A-25)-(A-32) float_t w_lat10(delta_phi / (igp[1].latitude_deg - igp[2].latitude_deg)), // a.k.a. y_pp w_lat23(1. - w_lat10), w_lng0((delta_lambda + igp[2].delta_lng(igp[1])) / igp[0].delta_lng(igp[1])), w_lng3(delta_lambda / igp[3].delta_lng(igp[2])); // a.k.a. x_pp // res = (w_lng0 * [0] + (1. - w_lng0) * [1]) * w_lat10 + ((1. - w_lng3) * [2] + w_lng3 * [3]) * w_lat23; weight[0] = w_lng0 * w_lat10; weight[1] = (1. - w_lng0) * w_lat10; weight[2] = (1. - w_lng3) * w_lat23; weight[3] = w_lng3 * w_lat23; } void compute_weight_pole(const float_t &delta_phi, const float_t &delta_lambda){ float_t y_pp(delta_phi * ((delta_phi < 0) ? -1 : 1) / 10), // (A-33) x_pp((1. - y_pp * 2) * (delta_lambda / 90) + y_pp), // (A-34) x_pp_inv(1. - x_pp), y_pp_inv(1. - y_pp); weight[0] = x_pp * y_pp; weight[1] = x_pp_inv * y_pp; weight[2] = x_pp_inv * y_pp_inv; weight[3] = x_pp * y_pp_inv; } /** * @return If extrapolation occurs, false is returned; otherwise true. */ bool compute_weight_three(const float_t &delta_phi, const float_t &delta_lambda, const int_t &skip){ float_t y_pp(delta_phi / (igp[1].latitude_deg - igp[2].latitude_deg)), x_pp(delta_lambda / igp[3].delta_lng(igp[2])); switch(skip){ // assignment rule: sum is 1, weight of non-diagonal point is remain? case 0: weight[0] = 0; weight[1] = y_pp; weight[2] = 1. - x_pp - y_pp; weight[3] = x_pp; if(weight[2] < 0){return false;} break; case 1: weight[0] = y_pp; weight[1] = 0; weight[2] = 1. - x_pp; weight[3] = x_pp - y_pp; if(weight[3] < 0){return false;} break; case 2: weight[0] = x_pp + y_pp - 1; weight[1] = 1. - x_pp; weight[2] = 0; weight[3] = 1. - y_pp; if(weight[0] < 0){return false;} break; case 3: default: weight[0] = x_pp; weight[1] = y_pp - x_pp; weight[2] = 1. - y_pp; weight[3] = 0; if(weight[1] < 0){return false;} break; } return true; } /** * @return If three point interpolation is successfully prepared, true; otherwise false. */ bool compute_weight_three(const float_t &delta_phi, const float_t &delta_lambda){ for(int i(0); i <= 3; i++){ if(!checked[i]){ // automatically find unavailable point return compute_weight_three(delta_phi, delta_lambda, i); } } return false; } PointProperty compute_property( #if defined(SWIG) // work around for SWIG parser error const typename PointProperty::raw_t *selected #else const typename PointProperty::raw_t *(&selected)[4] #endif ){ float_t delay_raw(0), sigma2(0); bool use_sigma(true); for(int i(0); i <= 3; i++){ if(!checked[i]){continue;} delay_raw += weight[i] * selected[i]->delay; if(selected[i]->error_indicator == PointProperty::raw_t::ERROR_INDICATOR_NOT_MONITORED){ use_sigma = false; }else{ sigma2 += weight[i] * PointProperty::raw_t::raw2sigma2(selected[i]->error_indicator); } } PointProperty res = { PointProperty::raw_t::raw2delay(delay_raw), use_sigma ? sigma2 : PointProperty::raw_t::raw2sigma2(PointProperty::raw_t::ERROR_INDICATOR_NOT_MONITORED), }; return res; } static trapezoid_t generate_rectangle(const position_t &pivot, const int_t &delta_lat = 5, const int_t &delta_lng = 5){ int_t lng(pivot.longitude_deg + delta_lng); if(lng >= 180){lng -= 360;} trapezoid_t res = {{ {pivot.latitude_deg + delta_lat, lng}, {pivot.latitude_deg + delta_lat, pivot.longitude_deg}, pivot, {pivot.latitude_deg, lng}, }, { false, false, false, false, }}; return res; } static trapezoid_t generate_rectangle_pole(const position_t &pivot){ int_t lng0(pivot.longitude_deg - 180), lng1(pivot.longitude_deg - 90), lng3(pivot.longitude_deg + 90); trapezoid_t res = {{ {pivot.latitude_deg, (lng0 < -180) ? (lng0 + 360) : lng0}, {pivot.latitude_deg, (lng1 < -180) ? (lng1 + 360) : lng1}, pivot, {pivot.latitude_deg, (lng3 >= 180) ? (lng3 - 360) : lng3}, }, { false, false, false, false, }}; return res; } /** * Get expanded rectangle * * @param delta_lat When positive, move a parallel between igp[1] and igp[0] toward the nearer pole; * when negative, move a parallel between igp[2] and igp[3] toward the other pole. * Be careful, when negative, the difference of IPP from pivot, i.e. igp[2], should be recalculated. * * @param delta_lng When positive, move a meridian between igp[0] and igp[3] east; * when negative, move a meridian between igp[1] and igp[2] west. * Be careful, when negative, the difference of IPP from pivot, i.e. igp[2], should be recalculated. * * @return Expanded rectangle */ trapezoid_t expand_rectangle(const int_t &delta_lat, const int_t &delta_lng) const { trapezoid_t res(*this); if(delta_lat != 0){ int_t delta_lat2(delta_lat * ((res.igp[1].latitude_deg >= 0) ? 1 : -1)); // check hemisphere if(delta_lat > 0){ res.igp[1].latitude_deg = (res.igp[0].latitude_deg += delta_lat2); res.checked[1] = res.checked[0] = false; }else{ res.igp[2].latitude_deg = (res.igp[3].latitude_deg += delta_lat2); res.checked[2] = res.checked[3] = false; } } if(delta_lng > 0){ res.igp[0].longitude_deg += delta_lng; if(res.igp[0].longitude_deg >= 180){res.igp[0].longitude_deg -= 360;} res.igp[3].longitude_deg = res.igp[0].longitude_deg; res.checked[3] = res.checked[0] = false; }else if(delta_lng < 0){ res.igp[1].longitude_deg += delta_lng; if(res.igp[1].longitude_deg < -180){res.igp[1].longitude_deg += 360;} res.igp[2].longitude_deg = res.igp[1].longitude_deg; res.checked[2] = res.checked[1] = false; } return res; } }; protected: typename PointProperty::raw_t properties[position_index_t::LAT_INDEX_MAX + 1][position_index_t::LNG_INDEX_MAX + 1]; public: template T check_availability_hook(trapezoid_t &in, const T &out) const { return out; // for debug } /** * @return available IGP(s) */ int_t check_availability(trapezoid_t &target, #if defined(SWIG) // work around for SWIG parser error const typename PointProperty::raw_t *cache #else const typename PointProperty::raw_t *(&cache)[4] #endif ) const { int_t res(0); for(int i(0); i < 4; ++i){ if(target.checked[i]){res++; continue;} position_index_t index(target.igp[i]); if((cache[i] = &properties[index.lat_index][index.lng_index])->is_available()){ target.checked[i] = true; res++; } } return check_availability_hook(target, res); } /** * Select appropriate grids and perform interpolation with the selected grids * * @param latitude_deg Latitude in degrees * @param longitude_deg Longitude in degrees * @return Interpolated result; if interpolation fails, PointProperty::unavailable will be returned. * @see A.4.4.10.2, A.4.4.10.3 */ PointProperty interpolate(const float_t &latitude_deg, const float_t &longitude_deg) const { pivot_t pivot(get_pivot(latitude_deg, longitude_deg)); const typename PointProperty::raw_t *selected[4]; bool north_hemisphere(latitude_deg >= 0); int_t lat_deg_abs(pivot.igp.latitude_deg * (north_hemisphere ? 1 : -1)); if(lat_deg_abs <= 55){ trapezoid_t rect_5_5(trapezoid_t::generate_rectangle(pivot.igp, north_hemisphere ? 5 : -5, 5)); // A4.4.10.2 a-1) switch(check_availability(rect_5_5, selected)){ case 4: // a-1) rect_5_5.compute_weight(pivot.delta.latitude_deg, pivot.delta.longitude_deg); return rect_5_5.compute_property(selected); case 3: // a-2) if(rect_5_5.compute_weight_three(pivot.delta.latitude_deg, pivot.delta.longitude_deg)){ return rect_5_5.compute_property(selected); } } struct { trapezoid_t rect; float_t delta_lat, delta_lng; int_t availability; } rect_10_10[] = { // A4.4.10.2 a-3), 5x5 => 10x10 {rect_5_5.expand_rectangle( 5, 5), pivot.delta.latitude_deg, pivot.delta.longitude_deg}, {rect_5_5.expand_rectangle( 5, -5), pivot.delta.latitude_deg, pivot.delta.longitude_deg + 5}, {rect_5_5.expand_rectangle(-5, 5), pivot.delta.latitude_deg + (north_hemisphere ? 5 : -5), pivot.delta.longitude_deg}, {rect_5_5.expand_rectangle(-5, -5), pivot.delta.latitude_deg + (north_hemisphere ? 5 : -5), pivot.delta.longitude_deg + 5}, }; for(int i(0); i < 4; ++i){ // a-3) four point interpolation if((lat_deg_abs == 55) && (rect_10_10[i].rect.igp[1].latitude_deg * (north_hemisphere ? 1 : -1) == 65) && ((rect_10_10[i].rect.igp[1].longitude_deg + 180) % 10 != 0)){ // When pivot lat = 55, -55, one 10x10 trapezoids are unable to be formed, // because of lack of grid points at lat = 65, -65. rect_10_10[i].availability = 0; continue; } if((rect_10_10[i].availability = check_availability(rect_10_10[i].rect, selected)) == 4){ rect_10_10[i].rect.compute_weight(rect_10_10[i].delta_lat, rect_10_10[i].delta_lng); return rect_10_10[i].rect.compute_property(selected); } } for(int i(0); i < 4; ++i){ // a-4) three point interpolation if((rect_10_10[i].availability == 3) && rect_10_10[i].rect.compute_weight_three(rect_10_10[i].delta_lat, rect_10_10[i].delta_lng)){ return rect_10_10[i].rect.compute_property(selected); } } }else if(lat_deg_abs <= 70){ trapezoid_t rect_5_10(trapezoid_t::generate_rectangle(pivot.igp, north_hemisphere ? 5 : -5, 10)); // A4.4.10.2 b-1) switch(check_availability(rect_5_10, selected)){ case 4: // b-1) rect_5_10.compute_weight(pivot.delta.latitude_deg, pivot.delta.longitude_deg); return rect_5_10.compute_property(selected); case 3: // b-2) if(rect_5_10.compute_weight_three(pivot.delta.latitude_deg, pivot.delta.longitude_deg)){ return rect_5_10.compute_property(selected); } } struct { trapezoid_t rect; float_t delta_lat, delta_lng; int_t availability; } rect_10_10[] = { // A4.4.10.2 b-3) , 5x10 => 10x10 {rect_5_10.expand_rectangle( 5, 0), pivot.delta.latitude_deg, pivot.delta.longitude_deg}, {rect_5_10.expand_rectangle(-5, 0), pivot.delta.latitude_deg + (north_hemisphere ? 5 : -5), pivot.delta.longitude_deg}, }; for(int i(0); i < 2; ++i){ // b-3) four point interpolation if((lat_deg_abs == 70) && (rect_10_10[i].rect.igp[1].latitude_deg * (north_hemisphere ? 1 : -1) == 80)){ // When pivot lat = 70, -70, one 10x10 trapezoids are unable to be formed, // because of no grid point at lat = 80, -80. rect_10_10[i].availability = 0; continue; } if((rect_10_10[i].availability = check_availability(rect_10_10[i].rect, selected)) == 4){ rect_10_10[i].rect.compute_weight(rect_10_10[i].delta_lat, rect_10_10[i].delta_lng); return rect_10_10[i].rect.compute_property(selected); } } for(int i(0); i < 2; ++i){ // b-4) three point interpolation if((rect_10_10[i].availability == 3) && rect_10_10[i].rect.compute_weight_three(rect_10_10[i].delta_lat, rect_10_10[i].delta_lng)){ return rect_10_10[i].rect.compute_property(selected); } } }else if(lat_deg_abs <= 75){ trapezoid_t rect_10_10(trapezoid_t::generate_rectangle(pivot.igp, north_hemisphere ? 10 : -10, 10)); // maximum 4 kinds of trial // 1) 10x30, both 85 points are band 9-10 (30 deg separation) // 2,3) 10X30, one 85 point is in band 0-8, the other is in band 9-10 // 4) 10x90, both 85 points are band 0-8 (90 deg separation) int_t lng_85_west_low_band, lng_85_west_high_band; int_t lng_85_east_low_band, lng_85_east_high_band; { int_t lng_reg(pivot.igp.longitude_deg + 180); // [-180, 180) => [0, 360) if(north_hemisphere){ lng_85_west_low_band = (lng_reg / 30 * 30) - 180; // W180, W150, ... lng_85_west_high_band = (lng_reg / 90 * 90) - 180; // W180, W90, ... }else{ lng_85_west_low_band = (lng_reg < 10) ? 160 : (((lng_reg - 10) / 30) * 30 - 170); // W170, W140, ..., E160 lng_85_west_high_band = (lng_reg < 40) ? 130 : (((lng_reg - 40) / 90) * 90 - 140); // W140, W50, ..., E130 } lng_85_east_low_band = lng_85_west_low_band + 30; lng_85_east_high_band = lng_85_west_high_band + 90; if(lng_85_east_low_band >= 180){lng_85_east_low_band -= 360;} if(lng_85_east_high_band >= 180){lng_85_east_high_band -= 360;} } { // check 1) rect_10_10.igp[1].longitude_deg = lng_85_west_low_band; rect_10_10.igp[0].longitude_deg = lng_85_east_low_band; if(check_availability(rect_10_10, selected) == 4){ rect_10_10.compute_weight(pivot.delta.latitude_deg, pivot.delta.longitude_deg); return rect_10_10.compute_property(selected); } } if(rect_10_10.checked[2] && rect_10_10.checked[3]){ // Requirement: lower latitude point information is broadcasted. bool check_again(true); do{ if(lng_85_west_low_band == lng_85_west_high_band){ // |[1]<--(30)-->[0]|----(90)---->| if(rect_10_10.checked[1]){ // prepare for the last trial rect_10_10.igp[0].longitude_deg = lng_85_east_high_band; //rect_10_10.checked[0] = false; // already set }else{ check_again = false; } break; } if(lng_85_east_low_band == lng_85_east_high_band){ // |<----(90)----|[1]<--(30)-->[0]| if(rect_10_10.checked[0]){ // prepare for the last trial rect_10_10.igp[1].longitude_deg = lng_85_west_high_band; //rect_10_10.checked[1] = false; // already set }else{ check_again = false; } break; } // just middle case: |<--(90)--|[1]<--(30)-->[0]|---->| if(!rect_10_10.checked[0]){ // check 2) |<--(90)--|[1]<--(30)-->[0]|---->[0]'| rect_10_10.igp[0].longitude_deg = lng_85_east_high_band; //rect_10_10.checked[0] = false; // already set, 1st trial } if(!rect_10_10.checked[1]){ // check 3) |[1]'<--(90)--|[1]<--(30)-->[0]|---->| rect_10_10.igp[1].longitude_deg = lng_85_west_high_band; //rect_10_10.checked[1] = false; // already set, 1st trial } }while(false); // check 2-4) if(check_again && (check_availability(rect_10_10, selected) == 4)){ rect_10_10.compute_weight(pivot.delta.latitude_deg, pivot.delta.longitude_deg); return rect_10_10.compute_property(selected); } } }else{ // pole trapezoid_t rect(trapezoid_t::generate_rectangle_pole(pivot.igp)); if(check_availability(rect, selected) == 4){ rect.compute_weight_pole(pivot.delta.latitude_deg, pivot.delta.longitude_deg); return rect.compute_property(selected); } } // Correction unavailable return PointProperty::unavailable; } protected: static const u8_t IODI_INVALID = 4; // valid value ranges from 0 to 3. struct { u8_t iodi; typename DataBlock::Type18::mask_t mask; void clear() { iodi = IODI_INVALID; mask.valid = 0; } } masks[11], masks_new[11]; // "masks" for normal use, "masks_new" for temporal use for iodi transition /** * Update mask and IGPs based on new mask having new IODI * @param band band number * @see 2.1.4.9.3 "The equipment shall be able to store and use two IGP masks ..." */ void transit_to_new_mask(const u8_t &band) { // remove points which is not activated in the new mask typename DataBlock::Type18::mask_t &mask_old(masks[band].mask), &mask_new(masks_new[band].mask); for(u8_t i(0), j(0); i < mask_old.valid; ++i){ bool still_use(false); for(; j < mask_new.valid; ++j){ if(mask_old.linear[i] < mask_new.linear[j]){ break; } if(mask_old.linear[i] == mask_new.linear[j]){ still_use = true; ++j; break; } } if(still_use){continue;} position_index_t index(position(band, mask_old.linear[i])); properties[index.lat_index][index.lng_index] = PointProperty::raw_t::unavailable; } masks[band] = masks_new[band]; masks_new[band].clear(); } void clear_igp() { for(unsigned int i(0); i < sizeof(properties) / sizeof(properties[0]); ++i){ for(unsigned int j(0); j < sizeof(properties[0]) / sizeof(properties[0][0]); ++j){ properties[i][j] = PointProperty::raw_t::unavailable; } } } void clear_mask(){ for(unsigned int i(0); i < sizeof(masks) / sizeof(masks[0]); ++i){ masks[i].clear(); } for(unsigned int i(0); i < sizeof(masks_new) / sizeof(masks_new[0]); ++i){ masks_new[i].clear(); } } public: /** * Update mask * @param band IGP band * @param iodi_new Issue of data, ionospheric * @param mask_new New mask * @return True if mask is up to date, otherwise false. */ bool update_mask(const u8_t &band, const u8_t &iodi_new, const typename DataBlock::Type18::mask_t &mask_new){ if((masks[band].iodi == iodi_new) || (masks_new[band].iodi == iodi_new)){ // lazy decline, because the same iodi means up to date return true; } if(masks[band].iodi == IODI_INVALID){ masks[band].iodi = iodi_new; masks[band].mask = mask_new; return true; } if(masks_new[band].iodi == IODI_INVALID){ masks_new[band].iodi = iodi_new; masks_new[band].mask = mask_new; return true; } return false; } /** * Update mask with broadcasted data * @param type18 Type 18 message * @return True if mask is updated and changed, otherwise false. */ template bool update_mask(const Input *type18){ typedef typename DataBlock::Type18 msg_t; u8_t band(msg_t::band(type18)); return update_mask(band, msg_t::iodi(type18), msg_t::mask(type18, band)); } /** * Register new ionospheric grind point property * @param IGP position * @param prop New property * @return Always true */ bool register_igp(const position_t &pos, const typename PointProperty::raw_t &prop){ position_index_t index(pos); properties[index.lat_index][index.lng_index] = prop; return true; } /** * Register new properties of ionospheric grid points (IGPs) with broadcasted data * @param type26 Type 26 message * @return True if IGPs are registered, otherwise false */ template bool register_igp(const InputT *type26){ typedef typename DataBlock::Type26 msg_t; u8_t band(msg_t::band(type26)), iodi(msg_t::iodi(type26)); if(masks[band].iodi != iodi){ if(masks_new[band].iodi != iodi){ return false; } // Change mask due to new arrival of IODI transit_to_new_mask(band); } u8_t *mask_pos(masks[band].mask.block[msg_t::block_id(type26)]); int i_max(masks[band].mask.valid - (mask_pos - masks[band].mask.linear)); if(i_max > DataBlock::Type18::mask_t::each_block){ i_max = DataBlock::Type18::mask_t::each_block; } for(int i(0); i < i_max; ++i, ++mask_pos){ register_igp(position(band, *mask_pos), PointProperty::raw_t::fetch(type26, i)); } return true; } IonosphericGridPoints(){ clear_igp(); clear_mask(); } virtual ~IonosphericGridPoints(){} /** * Print delay map with ASCII characters */ friend std::ostream &operator<<(std::ostream &out, const IonosphericGridPoints &igp){ static const char base32_chr[] = "0123456789ABCdEFGHiJKLMNoPQRSTUV"; // base 32 // the first line out << " "; for(int j(0); j < sizeof(igp.properties[0]) / sizeof(igp.properties[0][0]); ++j){ int lng(position_index_t::idx2lng(j)); out << (lng == 0 ? '0' : (lng % 90 == 0 ? '|' : (lng % 30 == 0 ? '+' : ' '))); } out << std::endl; for(int i(0); i < sizeof(igp.properties) / sizeof(igp.properties[0]); ++i){ out.width(4); out << position_index_t::idx2lat(i) << ' '; for(int j(0); j < sizeof(igp.properties[0]) / sizeof(igp.properties[0][0]); ++j){ if(!igp.properties[i][j].is_available()){ out << ' '; }else{ out << base32_chr[igp.properties[i][j].delay >> 4]; // 0-510 => 0-31 } } out << std::endl; } return out; } /** * Calculate correction value in accordance with ionospheric model * * @param relative_pos satellite position (relative position, NEU) * @param usrllh user position (absolute position, LLH) * @return correction in meters * @see A.4.4.10 */ PointProperty iono_correction( const enu_t &relative_pos, const llh_t &usrllh) const { // A.4.4.10.1 Pierce point calculation typename gps_space_node_t::pierce_point_res_t pp(gps_space_node_t::pierce_point(relative_pos, usrllh)); // A.4.4.10.2 IGP selection, and A.4.4.10.3 Interpolation PointProperty prop(interpolate(pp.latitude / M_PI * 180, pp.longitude / M_PI * 180)); if(prop.is_available()){ // A.4.4.10.4 Compute slant delay float_t fpp(gps_space_node_t::slant_factor(relative_pos)); prop.delay *= fpp; // (A-41) prop.sigma2 *= (fpp * fpp); // (A-43) } return prop; } }; class IonosphericGridPoints_with_Timeout : public IonosphericGridPoints { protected: gps_time_t t_last_mask; gps_time_t t_last_correction; bool is_mask_timeout(const gps_time_t &t_reception, const bool &LNAV_VNAV_LP_LPV_approach){ float_t delta_t(t_last_mask.interval(t_reception)); return LNAV_VNAV_LP_LPV_approach ? (delta_t >= Timing::values[Timing::IONOSPHERIC_GRID_MASK].timeout_LNAV_VNAV_LP_LPV_approach) : (delta_t >= Timing::values[Timing::IONOSPHERIC_GRID_MASK].timeout_EN_Route_Terminal_LNAV); } bool is_correction_timeout(const gps_time_t &t_reception, const bool &LNAV_VNAV_LP_LPV_approach){ float_t delta_t(t_last_correction.interval(t_reception)); return LNAV_VNAV_LP_LPV_approach ? (delta_t >= Timing::values[Timing::IONOSPHERIC_CORRECTIONS].timeout_LNAV_VNAV_LP_LPV_approach) : (delta_t >= Timing::values[Timing::IONOSPHERIC_CORRECTIONS].timeout_EN_Route_Terminal_LNAV); } public: IonosphericGridPoints_with_Timeout() : IonosphericGridPoints(), t_last_mask(0, 0), t_last_correction(0, 0) {} using IonosphericGridPoints::update_mask; using IonosphericGridPoints::register_igp; using IonosphericGridPoints::iono_correction; template bool update_mask( const Input *type18, const gps_time_t &t_reception, const bool &LNAV_VNAV_LP_LPV_approach = false){ if(is_mask_timeout(t_reception, LNAV_VNAV_LP_LPV_approach)){ IonosphericGridPoints::clear_mask(); } bool res(update_mask(type18)); if(res){ t_last_mask = t_reception; } return res; } template bool register_igp( const InputT *type26, const gps_time_t &t_reception, const bool &LNAV_VNAV_LP_LPV_approach = false){ if(is_mask_timeout(t_reception, LNAV_VNAV_LP_LPV_approach)){ IonosphericGridPoints::clear_mask(); return false; } if(is_correction_timeout(t_reception, LNAV_VNAV_LP_LPV_approach)){ IonosphericGridPoints::clear_igp(); } bool res(register_igp(type26)); if(res){ t_last_correction = t_reception; } return res; } typename IonosphericGridPoints::PointProperty iono_correction( const enu_t &relative_pos, const llh_t &usrllh, const gps_time_t &t, const bool &LNAV_VNAV_LP_LPV_approach = false) const { if(is_correction_timeout(t, LNAV_VNAV_LP_LPV_approach)){ return IonosphericGridPoints::PointProperty::unavailable; } return iono_correction(relative_pos, usrllh); } }; /** * Calculate Sagnac correction range in meter, which must be accounted * for residual calculation of pseudo range. * * @param sat_pos Satellite position * @param usr_pos User position * @return correction range * @see A.4.4.11 * @see SBAS_SpaceNode::Satellite::Ephemeris::constellation */ static float_t sagnac_correction( const xyz_t sat_pos, const xyz_t usr_pos) { return WGS84::Omega_Earth_IAU * (sat_pos.x() * usr_pos.y() - sat_pos.y() * usr_pos.x()) / gps_space_node_t::light_speed; } /** * Calculate correction value in accordance with tropospheric model * * @param year_utc UTC floating-point year * @param relative_pos satellite position (relative position, NEU) * @param usrllh user position (absolute position, LLH) * @see A.4.2.4 * @return correction in meters */ static float_t tropo_correction( const float_t &year_utc, const enu_t &relative_pos, const llh_t &usrllh){ if(usrllh.height() > 10E3){ // same as RTKlib; troposphere ranges from 0 to approximately 11km return 0; } union MeteologicalParameter { struct { float_t p, T, e, beta, lambda; // mbar, K, mbar, K/m, [dimless] }; float_t v[5]; }; static const struct { MeteologicalParameter average, seasonal_variation; } preset[] = { {{1013.25, 299.65, 26.31, 6.30E-3, 2.77}, { 0.00, 0.00, 0.00, 0.00E-3, 0.00}}, // 15 {{1017.25, 294.15, 21.79, 6.05E-3, 3.15}, {-3.75, 7.00, 8.85, 0.25E-3, 0.33}}, // 30 {{1015.75, 283.15, 11.66, 5.58E-3, 2.57}, {-2.25, 11.00, 7.24, 0.32E-3, 0.46}}, // 45 {{1011.75, 272.15, 6.78, 5.39E-3, 1.81}, {-1.75, 15.00, 5.36, 0.81E-3, 0.74}}, // 60 {{1013.00, 263.65, 4.11, 4.53E-3, 1.55}, {-0.50, 14.50, 3.39, 0.62E-3, 0.30}}, // 75 }; // Table A-2 static const int preset_langth(sizeof(preset) / sizeof(preset[0])); float_t preset_idx_f(std::abs(usrllh.latitude()) / (M_PI / 180 * 15)); int preset_idx(preset_idx_f); MeteologicalParameter average, seasonal_variation; if(preset_idx == 0){ average = preset[preset_idx].average; seasonal_variation = preset[preset_idx].seasonal_variation; }else if(preset_idx >= (preset_langth - 1)){ average = preset[preset_langth - 1].average; seasonal_variation = preset[preset_langth - 1].seasonal_variation; }else{ // linear interpolation float_t weight_b(preset_idx_f - preset_idx), weight_a(1. - weight_b); for(std::size_t j(0); j < sizeof(average.v) / sizeof(average.v[0]); ++j){ average.v[j] = preset[preset_idx].average.v[j] * weight_a + preset[preset_idx + 1].average.v[j] * weight_b; // (A-4) seasonal_variation.v[j] = preset[preset_idx].seasonal_variation.v[j] * weight_a + preset[preset_idx + 1].seasonal_variation.v[j] * weight_b; // (A-5) } } float_t d_hyd, d_wet; { // (A-3) MeteologicalParameter param; { float_t Dmin_year(((usrllh.latitude() < 0) ? 211 : 28) / 365.25); float_t year_int; float_t k(std::cos(M_PI * 2 * (std::modf(year_utc, &year_int) - Dmin_year))); for(std::size_t j(0); j < sizeof(param.v) / sizeof(param.v[0]); ++j){ param.v[j] = average.v[j] - seasonal_variation.v[j] * k; } } static const float_t k1(77.604), k2(382000), Rd(287.054), gm(9.784); // K/mbar, K^2/mbar, J/(kg*K), m/s^2 // Zero-altitude zenith delay term (z_hyd, z_wet) float_t z_hyd(1E-6 * k1 * Rd * param.p / gm), // (A-6) z_wet(1E-6 * k2 * Rd / (gm * (param.lambda + 1) - param.beta * Rd) * param.e / param.T); // (A-7) { const float_t &h(usrllh.height()); // Altitude (m) static const float_t g(9.80665); // m/s^2 if(h > 0){ float_t x(1. - (param.beta * h / param.T)), y(g / Rd / param.beta); d_hyd = std::pow(x, y) * z_hyd; // (A-8) d_wet = std::pow(x, y * (param.lambda + 1) - 1) * z_wet; // (A-9) }else{ d_hyd = z_hyd; d_wet = z_wet; } } } float_t m_el; { // Elevation (rad) float_t el(relative_pos.elevation()); m_el = 1.001 / std::sqrt(0.002001 + std::pow(std::sin(el), 2)); // (A-10a) } return -(d_hyd + d_wet) * m_el; } /** * UTC parameters * */ struct UTC_Parameters { float_t A1; ///< UTC parameter for SBAS network time (s/s) float_t A0; ///< UTC parameter for SBAS network time (s) uint_t t_ot; ///< Epoch time (UTC) (s) uint_t WN_t; ///< Epoch time (UTC) (weeks) int_t delta_t_LS; ///< Current leap seconds (s) uint_t WN_LSF; ///< Last leap second update week (weeks) uint_t DN; ///< Last leap second update day (days) int_t delta_t_LSF; ///< Updated leap seconds (s) struct raw_t { s32_t A1; ///< UTC parameter (-50, s/s) s32_t A0; ///< UTC parameter (-30, s) u8_t t_ot; ///< Epoch time (UTC) (12, s) u8_t WN_t; ///< Epoch time (UTC) (weeks, truncated) s8_t delta_t_LS; ///< Current leap seconds (s) u8_t WN_LSF; ///< Last leap second update week (weeks, truncated) u8_t DN; ///< Last leap second update day (days) s8_t delta_t_LSF; ///< Updated leap seconds (s) template static raw_t fetch(const InputT *buf){ typedef typename DataBlock::Type12 msg_t; raw_t res = { msg_t::A1_SNT(buf), msg_t::A0_SNT(buf), msg_t::t_ot(buf), msg_t::WN_t(buf), msg_t::delta_t_LS(buf), msg_t::WN_LSF(buf), msg_t::DN(buf), msg_t::delta_t_LSF(buf), }; return res; } enum { SF_A1, SF_A0, SF_NUM, }; static const float_t sf[SF_NUM]; operator UTC_Parameters() const { UTC_Parameters converted; #define CONVERT(TARGET) \ {converted.TARGET = sf[SF_ ## TARGET] * TARGET;} CONVERT(A1); CONVERT(A0); converted.t_ot = ((uint_t)t_ot) << 12; converted.WN_t = WN_t; converted.delta_t_LS = delta_t_LS; converted.WN_LSF = WN_LSF; converted.DN = DN; converted.delta_t_LSF = delta_t_LSF; #undef CONVERT return converted; }; }; }; class SatelliteProperties { public: typedef typename gps_space_node_t::SatelliteProperties::constellation_t constellation_t; /** * SBAS Ephemeris * @see Table A-18 */ struct Ephemeris { uint_t svid; ///< Satellite number uint_t WN; ///< Week number float_t t_0; ///< Time of applicability (s) <= time of a week int_t URA; ///< User range accuracy (index) float_t x, y, z; ///< ECEF position (m) float_t dx, dy, dz; ///< ECEF velocity (m/s) float_t ddx, ddy, ddz; ///< ECEF acceleration (m/s^2) float_t a_Gf0; ///< Clock correction parameter (s) float_t a_Gf1; ///< Clock correction parameter (s/s) /** * Adjust time of ephemeris with time of current */ void adjust_time(const gps_time_t &t_current){ WN = t_current.week; float_t sec_of_a_day(std::fmod(t_current.seconds, gps_time_t::seconds_day)), t_0_orig(t_0); t_0 += (t_current.seconds - sec_of_a_day); // roll over check float_t delta(sec_of_a_day - t_0_orig); if(delta > (gps_time_t::seconds_day / 4 * 3)){ // 0 --> t_0 ---------(3/4)---------> current --> day t_0 += gps_time_t::seconds_day; // probably, current --> t_0 if(t_0 >= gps_time_t::seconds_week){ WN++; t_0 -= gps_time_t::seconds_week; } }else if(-delta > (gps_time_t::seconds_day / 4 * 3)){ // 0 --> current ---------(3/4)---------> t_0 --> day t_0 -= gps_time_t::seconds_day; // probably, t_0 --> current if(t_0 < 0){ WN--; t_0 += gps_time_t::seconds_week; } } } /** * Check availability * @param t target time * @return always true, because timeout, which is based on the reception time, * is the only way to make this ephemeris unavailable. * This class does not take the reception time into account. * @see 2.1.1.4.9, A.4.5.1.3.3 */ bool is_valid(const gps_time_t &t) const { return ((WN > 0) || (t_0 >= 0)); } /** * Check fitness based on time of applicability (t_0) of ephemeris * @param t target time * @return true when best fit, otherwise, false * @see A.4.5.1.3.3 (A-56) */ bool maybe_better_one_avilable(const gps_time_t &t) const { float_t delta_t(-t.interval(WN, t_0)); return (delta_t < 0) || (delta_t > Timing::values[Timing::GEO_NAVIGATION_DATA].interval); } float_t clock_error(const gps_time_t &t) const { float_t t_G(-t.interval(WN, 0)); // t_0 is expected to be modified as time of week return a_Gf0 + a_Gf1 * (t_G - t_0); // Eq.(A-45), delay is positive } float_t clock_error_dot(const gps_time_t &t) const { return a_Gf1; } constellation_t constellation( const gps_time_t &t_tx, const float_t &dt_transit = 0, const bool &with_velocity = true) const { float_t delta_t(-t_tx.interval(WN, t_0)), delta_t2(delta_t * delta_t / 2); constellation_t res = { xyz_t( x + dx * delta_t + ddx * delta_t2, y + dy * delta_t + ddy * delta_t2, z + dz * delta_t + ddz * delta_t2).after(dt_transit), // Eq. (A-44) xyz_t( dx + ddx * delta_t, dy + ddy * delta_t, dz + ddz * delta_t).after(dt_transit), }; /* Sagnac correction, which is expected to perform before geometric distance calculation, * can be skipped by using non-zero dt_transit. * This is because the return values is corrected to be along with the coordinate * at the reception time. * @see SBAS_SpaceNode::sagnac_correction */ return res; } struct raw_t { u8_t svid; ///< Satellite number u16_t t_0; ///< Time of applicability (16, s) [0,86384] <= time of a day u8_t URA; ///< User range accuracy s32_t x, y, z; ///< ECEF position (0.08(xy), 0.4(z) m) s32_t dx, dy, dz; ///< ECEF velocity (0.000625(xy), 0.004(z) m) s16_t ddx, ddy, ddz; ///< ECEF acceleration (0.0000125(xy), 0.0000625(z) m/s^2) s16_t a_Gf0; ///< Clock correction parameter (2^-31, s) s8_t a_Gf1; ///< Clock correction parameter (2^-40, s/s) template static raw_t fetch(const InputT *buf, const u8_t &sv_number = 0){ typedef typename DataBlock::Type9 msg_t; raw_t res = { sv_number, // svid msg_t::t0(buf), // t_0 msg_t::ura(buf), // URA msg_t::x(buf), msg_t::y(buf), msg_t::z(buf), // x, y, z msg_t::dx(buf), msg_t::dy(buf), msg_t::dz(buf), // dx, dy, dz msg_t::ddx(buf), msg_t::ddy(buf), msg_t::ddz(buf), // ddx, ddy, ddz msg_t::a_Gf0(buf), msg_t::a_Gf1(buf), // a_Gf0, a_Gf1 }; return res; } enum { SF_t_0, SF_xy, SF_z, SF_dxy, SF_dz, SF_ddxy, SF_ddz, SF_a_Gf0, SF_a_Gf1, SF_NUM, }; static const float_t sf[SF_NUM]; operator Ephemeris() const { Ephemeris converted; #define CONVERT2(TARGET, TARGET_SF) \ {converted.TARGET = sf[SF_ ## TARGET_SF] * TARGET;} #define CONVERT(TARGET) CONVERT2(TARGET, TARGET) converted.svid = svid; converted.WN = 0; // Week number (must be configured later) @see adjust_time converted.URA = URA; CONVERT(t_0); // Time of a day => time of a week (must be configured later) @see adjust_time CONVERT2(x, xy); CONVERT2(y, xy); CONVERT(z); CONVERT2(dx, dxy); CONVERT2(dy, dxy); CONVERT(dz); CONVERT2(ddx, ddxy); CONVERT2(ddy, ddxy); CONVERT(ddz); CONVERT(a_Gf0); CONVERT(a_Gf1); #undef CONVERT #undef CONVERT2 return converted; } raw_t &operator=(const Ephemeris &eph){ #define CONVERT3(TARGET_DST, TARGET_SRC, TARGET_SF) \ {TARGET_DST = (s32_t)((TARGET_SRC + 0.5 * sf[SF_ ## TARGET_SF]) / sf[SF_ ## TARGET_SF]);} #define CONVERT2(TARGET, TARGET_SF) CONVERT3(eph.TARGET, eph.TARGET, TARGET_SF) #define CONVERT(TARGET) CONVERT2(TARGET, TARGET) svid = eph.svid; URA = eph.URA; CONVERT3(t_0, std::fmod(t_0, gps_time_t::seconds_day), t_0); CONVERT2(x, xy); CONVERT2(y, xy); CONVERT(z); CONVERT2(dx, dxy); CONVERT2(dy, dxy); CONVERT(dz); CONVERT2(ddx, ddxy); CONVERT2(ddy, ddxy); CONVERT(ddz); CONVERT(a_Gf0); CONVERT(a_Gf1); #undef CONVERT #undef CONVERT2 #undef CONVERT3 return *this; } }; bool is_equivalent(const Ephemeris &eph) const { do{ if(WN != eph.WN){break;} if(URA != eph.URA){break;} #define CHECK2(TARGET, TARGET_SF) \ if(std::abs(TARGET - eph.TARGET) > raw_t::sf[raw_t::SF_ ## TARGET_SF]){break;} #define CHECK(TARGET) CHECK2(TARGET, TARGET) CHECK(t_0); CHECK2(x, xy); CHECK2(y, xy); CHECK(z); CHECK2(dx, dxy); CHECK2(dy, dxy); CHECK(dz); CHECK2(ddx, ddxy); CHECK2(ddy, ddxy); CHECK(ddz); CHECK(a_Gf0); CHECK(a_Gf1); #undef CHECK #undef CHECK2 return true; }while(false); return false; } gps_time_t base_time() const { return gps_time_t(WN, t_0); } }; struct Ephemeris_with_Timeout : public Ephemeris { gps_time_t t_reception; Ephemeris_with_Timeout() : Ephemeris(), t_reception(0, 0) {} /** * Constructor to convert Ephemeris * reception time is interpreted to be equivalent to time of applicability (t_0) of eph, * therefore, eph is assumed that its t_0, i.e., week number and time of week, * has already been adjusted. * @param eph Epehemris */ Ephemeris_with_Timeout(const Ephemeris &eph) : Ephemeris(eph), t_reception(eph.WN, eph.t_0) {} /** * Constructor to convert Ephemeris with reception time * reception time will be adjusted with time of reception. * @param eph Ephemeris * @param t_rx Reception time */ Ephemeris_with_Timeout(const Ephemeris &eph, const gps_time_t &t_rx) : Ephemeris(eph), t_reception(t_rx) { Ephemeris::adjust_time(t_rx); } /** * Check availability on EN_Route, Terminal, or LNAV * @param t target time * @return true when interval between message reception time * and current time is within timeout threshold, otherwise false. * @see 2.1.1.4.9, A.4.5.1.3.3 */ bool is_valid_EN_Route_Terminal_LNAV(const gps_time_t &t) const { float_t delta_t(t_reception.interval(t)); return delta_t < Timing::values[ Timing::GEO_NAVIGATION_DATA].timeout_EN_Route_Terminal_LNAV; } /** * Check availability on LNAV, VNAV, LP, or LPV approach * @param t target time * @return true when interval between message reception time * and current time is within timeout threshold, otherwise false. * @see 2.1.1.4.9, A.4.5.1.3.3 */ bool is_valid_LNAV_VNAV_LP_LPV_approach(const gps_time_t &t) const { float_t delta_t(t_reception.interval(t)); return delta_t < Timing::values[ Timing::GEO_NAVIGATION_DATA].timeout_LNAV_VNAV_LP_LPV_approach; } /** * Return reception time as base time, which is different from non-timeout version for time of applicability. * This function will be used to sort multiple ephemeris in order of reception time. * @see Ephemeris::base_time() */ gps_time_t base_time() const { return t_reception; } }; /** * SBAS almanac * @see Table A-19 */ struct Almanac { uint_t data_id; uint_t prn; ///< PRN number uint_t SV_health; ///< Health status float_t x, y, z; ///< ECEF position (m) float_t dx, dy, dz; ///< ECEF velocity (m/s) float_t t_0; ///< Time of applicability (s) ///< Up-cast to ephemeris operator Ephemeris() const { Ephemeris converted = { prn, // Satellite number t_0, // Time of applicability (s) -1, // User range accuracy (index) x, y, z, // ECEF position (m) dx, dy, dz, // ECEF velocity (m/s) 0, 0, 0, // ECEF acceleration (m/s^2) 0, // Clock correction parameter (s) 0, // Clock correction parameter (s/s) }; return converted; } struct raw_t { u8_t data_id; u8_t prn; ///< PRN number u8_t SV_health; ///< Health status s16_t x, y, z; ///< ECEF position (2600(xy), 26000(z), m) s8_t dx, dy, dz; ///< ECEF velocity (10(xy), 60(z), m/s) u16_t t_0; ///< Time of applicability (64, s) template static raw_t fetch(const InputT *buf, const uint_t &ch){ typedef typename DataBlock::Type17 msg_t; raw_t res = { msg_t::id(buf, ch), // data_id msg_t::prn(buf, ch), // prn msg_t::health_status(buf, ch), // SV_health msg_t::x(buf, ch), msg_t::y(buf, ch), msg_t::z(buf, ch), // x, y, z msg_t::dx(buf, ch), msg_t::dy(buf, ch), msg_t::dz(buf, ch), // dx, dy, dz msg_t::t0(buf), // t_0 }; return res; } enum { SF_xy, SF_z, SF_dxy, SF_dz, SF_t_0, SF_NUM, }; static const float_t sf[SF_NUM]; operator Almanac() const { Almanac converted; #define CONVERT2(TARGET, TARGET_SF) \ {converted.TARGET = sf[SF_ ## TARGET_SF] * TARGET;} #define CONVERT(TARGET) CONVERT2(TARGET, TARGET) converted.data_id = data_id; converted.prn = prn; converted.SV_health = SV_health; CONVERT2(x, xy); CONVERT2(y, xy); CONVERT(z); CONVERT2(dx, dxy); CONVERT2(dy, dxy); CONVERT(dz); CONVERT(t_0); #undef CONVERT #undef CONVERT2 return converted; } }; }; }; class Satellite : public SatelliteProperties { friend class SBAS_SpaceNode; public: typedef typename SatelliteProperties::Ephemeris_with_Timeout eph_t; typedef typename gps_space_node_t::template PropertyHistory eph_list_t; typedef IonosphericGridPoints_with_Timeout igp_t; protected: eph_list_t eph_history; igp_t igp; public: Satellite() : eph_history(), igp() { // setup first ephemeris as invalid one eph_t &eph_current(const_cast(eph_history.current())); eph_current.WN = 0; eph_current.t_0 = -1; } template void each_ephemeris( Functor &functor, const typename eph_list_t::each_mode_t &mode = eph_list_t::EACH_ALL) const { eph_history.each(functor, mode); } void register_ephemeris(const eph_t &eph, const int &priority_delta = 1){ eph_history.add(eph, priority_delta); } const eph_t &ephemeris() const { return eph_history.current(); } /** * Select appropriate ephemeris within registered ones. * * @param target_time time at measurement * @param LNAV_VNAV_LP_LPV_approach * @return if true, appropriate ephemeris is selected, otherwise, not selected. */ bool select_ephemeris( const gps_time_t &target_time, const bool &LNAV_VNAV_LP_LPV_approach = false){ bool (eph_t::*is_valid_func)(const gps_time_t &) const ( LNAV_VNAV_LP_LPV_approach ? &eph_t::is_valid_LNAV_VNAV_LP_LPV_approach : &eph_t::is_valid_EN_Route_Terminal_LNAV); return (ephemeris().*is_valid_func)(target_time) // conservative || eph_history.select(target_time, is_valid_func); } const igp_t &ionospheric_grid_points() const { return igp; } }; public: typedef std::map satellites_t; protected: satellites_t _satellites; public: SBAS_SpaceNode() : _satellites() { } ~SBAS_SpaceNode(){ _satellites.clear(); } const satellites_t &satellites() const { return _satellites; } Satellite &satellite(const int &prn) { return _satellites[prn]; } bool has_satellite(const int &prn) const { return _satellites.find(prn) != _satellites.end(); } void update_all_ephemeris(const gps_time_t &target_time) { for(typename satellites_t::iterator it(_satellites.begin()); it != _satellites.end(); ++it){ it->second.select_ephemeris(target_time); } } typedef std::vector > available_satellites_t; /** * Return available satellites * @param lng_deg longitude of user position * @return (available_satellites_t) available satellites, nearer is faster */ available_satellites_t available_satellites(const float_t &lng_deg) const { available_satellites_t res; typename KnownSatellites::list_t nearest(KnownSatellites::nearest_ordered(lng_deg)); for(typename KnownSatellites::list_t::const_iterator it(nearest.begin()); it != nearest.end(); ++it){ int prn((*it)->prn); if(!has_satellite(prn)){continue;} res.push_back(std::make_pair(prn, &(const_cast(this)->_satellites[prn]))); } return res; } template MessageType decode_message( const InputT *buf, const int &prn, const gps_time_t &t_reception, const bool &LNAV_VNAV_LP_LPV_approach = false){ MessageType message_type((MessageType)DataBlock::message_type(buf)); Satellite &sat(_satellites[prn]); switch(message_type){ case GEO_NAVIGATION: { // 9 typename Satellite::eph_t eph( Satellite::eph_t::raw_t::fetch(buf, prn), t_reception); sat.eph_history.add(eph); break; } case DEGRADATION_PARAMS: { // 10 DegradationFactors dfactor(DegradationFactors::raw_t::fetch(buf)); break; } case IONO_GRID_POINT_MASKS: // 18 sat.igp.update_mask(buf, t_reception, LNAV_VNAV_LP_LPV_approach); break; case IONO_DELAY_CORRECTION: // 26 if(!sat.igp.register_igp(buf, t_reception, LNAV_VNAV_LP_LPV_approach)){ message_type = UNSUPPORTED_MESSAGE; } break; case NULL_MESSAGES: // 63 break; default: message_type = UNSUPPORTED_MESSAGE; } return message_type; } }; template template typename SBAS_SpaceNode::KnownSatellites::list_t SBAS_SpaceNode::KnownSatellites::sort(T sorter){ static const typename SBAS_SpaceNode::RangingCode codes[] = { {120, 145, 01106, 5, "ASECNA (A-SBAS)"}, {121, 175, 01241, 5, "EGNOS (Eutelsat 5WB)"}, {122, 52, 00267, 143.5, "SPAN (INMARSAT 4F1)"}, {123, 21, 00232, 31.5, "EGNOS (ASTRA 5B)"}, //{124, 237, 01617, 0, "(Reserved)"}, {125, 235, 01076, -16, "SDCM (Luch-5A)"}, {126, 886, 01764, 63.9, "EGNOS (INMARSAT 4F2)"}, {127, 657, 00717, 55, "GAGAN (GSAT-8)"}, {128, 634, 01532, 83, "GAGAN (GSAT-10)"}, {129, 762, 01250, 127, "MSAS (QZS-3)"}, {130, 355, 00341, 140, "BDSBAS (G6)"}, {131, 1012, 00551, -117, "WAAS (Eutelsat 117West B)"}, {132, 176, 00520, 93.5, "GAGAN (GSAT-15)"}, {133, 603, 01731, -129, "WAAS (SES-15)"}, {134, 130, 00706, 91.5, "KASS (MEASAT-3D)"}, {135, 359, 01216, -125, "WAAS (Intelsat Galaxy 30)"}, {136, 595, 00740, 5, "EGNOS (HOTBIRD 13G)"}, {137, 68, 01007, 127, "MSAS (QZS-3)"}, {138, 386, 00450, 107.3, "WAAS (ANIK F1R)"}, //{139, 797, 00305, 0, "MSAS (QZS-7)"}, {140, 456, 01653, 95, "SDCM (Luch-5V)"}, {141, 499, 01411, 167, "SDCM (Luch-5A)"}, //{142, 883, 01644, 0, "(Unallocated)"}, {143, 307, 01312, 110.5, "BDSBAS (G3)"}, {144, 127, 01060, 80, "BDSBAS (G2)"}, //{145, 211, 01560, 0, "(Unallocated)"}, //{146, 121, 00035, 0, "(Unallocated)"}, {147, 118, 00355, 5, "ASECNA (A-SBAS)"}, {148, 163, 00335, -24.8, "ASAL (ALCOMSAT-1)"}, //{149, 628, 01254, 0, "(Unallocated)"}, //{150, 853, 01041, 0, "EGNOS"}, //{151, 484, 00142, 0, "(Unallocated)"}, //{152, 289, 01641, 0, "(Unallocated)"}, //{153, 811, 01504, 0, "(Unallocated)"}, //{154, 202, 00751, 0, "(Unallocated)"}, //{155, 1021, 01774, 0, "(Unallocated)"}, //{156, 463, 00107, 0, "(Unallocated)"}, //{157, 568, 01153, 0, "(Unallocated)"}, //{158, 904, 01542, 0, "(Unallocated)"}, }; ///< @see https://www.gps.gov/technical/prn-codes/L1-CA-PRN-code-assignments-2021-Jun.pdf list_t res; res.reserve(sizeof(codes) / sizeof(codes[0])); for(unsigned int i(0); i < sizeof(codes) / sizeof(codes[0]); ++i){ res.push_back(&codes[i]); } std::sort(res.begin(), res.end(), sorter); return res; } template const typename SBAS_SpaceNode::KnownSatellites::list_t SBAS_SpaceNode::KnownSatellites::prn_ordered = SBAS_SpaceNode::KnownSatellites::sort( typename SBAS_SpaceNode::RangingCode::prn_sorter_t()); template const typename SBAS_SpaceNode::KnownSatellites::list_t SBAS_SpaceNode::KnownSatellites::longitude_ordered = SBAS_SpaceNode::KnownSatellites::sort( typename SBAS_SpaceNode::RangingCode::lng_sorter_t()); template const typename SBAS_SpaceNode::KnownSatellites::list_t SBAS_SpaceNode::KnownSatellites::name_ordered = SBAS_SpaceNode::KnownSatellites::sort( typename SBAS_SpaceNode::RangingCode::name_sorter_t()); template const typename SBAS_SpaceNode::Timing::values_t SBAS_SpaceNode::Timing::values[SBAS_SpaceNode::Timing::NUM_OF_TIMING_ITEMS] = { { 6}, // DONT_USE_FOR_SAFETY_APPLICATIONS (0) {120, 600, 600}, // PRN_MASK (1) { 6, 18, 12}, // UDREI (2-6, 24) {}, // FAST_CORRECTIONS (2-5, 24) {120, 360, 240}, // LONG_TERM_CORRECTIONS (24, 25) {120, 360, 240}, // GEO_NAVIGATION_DATA (9) {120, 360, 240}, // FAST_CORRECTION_DEGRADATION (7) {120, 360, 240}, // DEGRADATION_PARAMETERS (10) {300, 1200, 1200}, // IONOSPHERIC_GRID_MASK (18) {300, 600, 600}, // IONOSPHERIC_CORRECTIONS (26) {300, 86400, 86400}, // UTC_TIMING_DATA (12) {300}, // ALNAMAC_DATA (17) {300, 86400, 86400}, // SERVICE_LEVEL (27) {120, 360, 240}, // CLOCK_EPHEMERIS_COVARIANCE_MATRIX (28) }; ///< @see Table A-25 template const typename SBAS_SpaceNode::IonosphericGridPoints::PointProperty::raw_t SBAS_SpaceNode::IonosphericGridPoints::PointProperty::raw_t::unavailable = { DELAY_DONT_USE, ERROR_INDICATOR_NOT_MONITORED, }; template const typename SBAS_SpaceNode::IonosphericGridPoints::PointProperty SBAS_SpaceNode::IonosphericGridPoints::PointProperty::unavailable = { 0, raw_t::raw2sigma2(raw_t::ERROR_INDICATOR_NOT_MONITORED), }; template SBAS_SpaceNode::IonosphericGridPoints::position_t::operator typename SBAS_SpaceNode::IonosphericGridPoints::position_index_t() const { SBAS_SpaceNode::IonosphericGridPoints::position_index_t res = { position_index_t::lat2idx(latitude_deg), position_index_t::lng2idx(longitude_deg)}; return res; } #define POWER_2(n) \ (((n) >= 0) \ ? (float_t)(1 << (n >= 0 ? n : 0)) \ : (((float_t)1) / (1 << (-(n) >= 30 ? 30 : -(n > 0 ? 0 : n))) \ / (1 << (-(n) >= 30 ? (-(n) - 30) : 0)))) template const typename SBAS_SpaceNode::float_t SBAS_SpaceNode::DegradationFactors::raw_t::sf[] = { 0.002, // SF_B_rcc 0.002, // SF_C_ltc_lsb 0.00005, // SF_C_ltc_v1 0.002, // SF_C_ltc_v0 0.0005, // SF_C_geo_lsb 0.00005, // SF_C_geo_v 0.5, // SF_C_er 0.001, // SF_C_iono_step 0.000005, // SF_C_iono_ramp 0.1, // SF_C_covariance }; template const typename SBAS_SpaceNode::float_t SBAS_SpaceNode::SatelliteProperties::Ephemeris::raw_t::sf[] = { 16, // SF_t_0 0.08, // SF_xy 0.4, // SF_z 0.000625, // SF_dxy 0.004, // SF_dz 0.0000125, // SF_ddxy 0.0000625, // SF_ddz POWER_2(-31), // SF_a_Gf0 POWER_2(-40), // SF_a_Gf1 }; template const typename SBAS_SpaceNode::float_t SBAS_SpaceNode::SatelliteProperties::Almanac::raw_t::sf[] = { 2600, // SF_xy 26000, // SF_z 10, // SF_dxy 60, // SF_dz 64, // SF_t_0 }; template const typename SBAS_SpaceNode::float_t SBAS_SpaceNode::UTC_Parameters::raw_t::sf[] = { POWER_2(-50), // SF_A1 POWER_2(-30), // SF_A0 }; #undef POWER_2 #endif /* __SBAS_H__ */