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gnss-sdr/src/core/system_parameters/GLONASS_L1_CA.h

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gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
/*!
* \file GLONASS_L1_CA.h
* \brief Defines system parameters for GLONASS L1 C/A signal and NAV data
* \author Damian Miralles, 2017. dmiralles2009(at)gmail.com
*
* -------------------------------------------------------------------------
*
* Copyright (C) 2010-2015 (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 <http://www.gnu.org/licenses/>.
*
* -------------------------------------------------------------------------
*/
#ifndef GNSS_SDR_GLONASS_L1_CA_H_
#define GNSS_SDR_GLONASS_L1_CA_H_
#include <vector>
#include <utility> // std::pair
#include "MATH_CONSTANTS.h"
#include "gnss_frequencies.h"
// Physical constants
const double GLONASS_C_m_s = SPEED_OF_LIGHT; //!< The speed of light, [m/s]
const double GLONASS_C_m_ms = 299792.4580; //!< The speed of light, [m/ms]
const double GLONASS_PI = 3.1415926535898; //!< Pi as defined in IS-GPS-200E
const double GLONASS_TWO_PI = 6.283185307179586; //!< 2Pi as defined in IS-GPS-200E
const double GLONASS_OMEGA_EARTH_DOT = 7.292115e-5; //!< Earth rotation rate, [rad/s]
gnav: Adding GLONASS GNAV Navigation Message Operations Adding code for navigation message computation for GLONASS GNAV code. Continues to fix the almanac position computation and fixes bugs in code due to compilation errors, coding style and Doxygen documentation
2017-06-21 04:44:44 +00:00
const double GLONASS_GM = 398600.4418e9; //!< Universal gravitational constant times the mass of the Earth, [m^3/s^2]
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
const double GLONASS_fM_a = 0.35e9; //!< Gravitational constant of atmosphere [m^3/s^2]
const double GLONASS_SEMI_MAJOR_AXIS = 6378136; //!< Semi-major axis of Earth [m]
const double GLONASS_FLATTENING = 1/29825784; //!< Flattening parameter
const double GLONASS_GRAVITY = 97803284; //!< Equatorial acceleration of gravity [mGal]
const double GLONASS_GRAVITY_CORRECTION = 0.87; //!< Correction to acceleration of gravity at sea-level due to Atmosphere[мGal]
const double GLONASS_J2 = 1082625.75e-9; //!< Second zonal harmonic of the geopotential
const double GLONASS_J4 = -2370.89e-9; //!<Fourth zonal harmonic of the geopotential
const double GLONASS_J6 = 6.08e-9; //!< Sixth zonal harmonic of the geopotential
const double GLONASS_J8 = 1.40e-11; //!< Eighth zonal harmonic of the geopotential
const double GLONASS_U0 = 62636861.4; //!< Normal potential at surface of common terrestrial ellipsoid [m^2/s^2]
const double GLONASS_C20 = -1082.63e-6; //!< Second zonal coefficient of spherical harmonic expansion
const double GLONASS_EARTH_RADIUS = 6378.136; //!< Equatorial radius of Earth [km]
gnav: Adding GLONASS GNAV Navigation Message Operations Adding code for navigation message computation for GLONASS GNAV code. Continues to fix the almanac position computation and fixes bugs in code due to compilation errors, coding style and Doxygen documentation
2017-06-21 04:44:44 +00:00
const double GLONASS_EARTH_INCLINATION = 0.000409148809899e3; //!< Mean inclination of ecliptic to equator (23 deg 26 min 33 sec) [rad]
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
gnav: Adding GLONASS GNAV Navigation Message Operations Adding code for navigation message computation for GLONASS GNAV code. Continues to fix the almanac position computation and fixes bugs in code due to compilation errors, coding style and Doxygen documentation
2017-06-21 04:44:44 +00:00
const double GLONASS_TAU_0 = -0.005835151531174e3; //!< (-334 deg 19 min 46.40 sec) [rad];
const double GLONASS_TAU_1 = 0.071018041257371e3; //!< (4069 deg 02 min 02.52 sec) [rad];
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
gnav: Adding GLONASS GNAV Navigation Message Operations Adding code for navigation message computation for GLONASS GNAV code. Continues to fix the almanac position computation and fixes bugs in code due to compilation errors, coding style and Doxygen documentation
2017-06-21 04:44:44 +00:00
const double GLONASS_MOON_Q0 = -0.001115184961435e3; //!< (-63 deg 53 min 43.41 sec) [rad]
const double GLONASS_MOON_Q1 = 8.328691103668023e3; //!< (477198 deg 50 min 56.79 sec) [rad]
const double GLONASS_MOON_OMEGA_0 = 0.004523601514852e3; //!< (259 deg 10 min 59.79 sec) [rad]
const double GLONASS_MOON_OMEGA_1 = -0.033757146246552e3; //!< (-1934 deg 08 min 31.23 sec) [rad]
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
const double GLONASS_MOON_GM = 4902.835; //!< Lunar gravitational constant [km^3/s^2]
const double GLONASS_MOON_SEMI_MAJOR_AXIS = 3.84385243e5; //!< Semi-major axis of lunar orbit [km];
const double GLONASS_MOON_ECCENTRICITY = 0.054900489; //!< Eccentricity of lunar orbit
gnav: Adding GLONASS GNAV Navigation Message Operations Adding code for navigation message computation for GLONASS GNAV code. Continues to fix the almanac position computation and fixes bugs in code due to compilation errors, coding style and Doxygen documentation
2017-06-21 04:44:44 +00:00
const double GLONASS_MOON_INCLINATION = 0.000089803977407e3; //!< Inclination of lunar orbit to ecliptic plane (5 deg 08 min 43.4 sec) [rad]
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
gnav: Adding GLONASS GNAV Navigation Message Operations Adding code for navigation message computation for GLONASS GNAV code. Continues to fix the almanac position computation and fixes bugs in code due to compilation errors, coding style and Doxygen documentation
2017-06-21 04:44:44 +00:00
const double GLONASS_SUN_OMEGA = 0.004908229466869e3; //!< TODO What is this operation in the seconds with T?(281 deg 13 min 15.0 + 6189.03*Т sec) [rad]
const double GLONASS_SUN_Q0 = 0.006256583774423e3; //!< (358 deg 28 min 33.04 sec) [rad]
const double GLONASS_SUN_Q1 = 0e3; //!< TODO Why is the value greater than 60?(129596579.10 sec) [rad]
const double GLONASS_SUN_GM = 0.1325263e12; //!< Solar gravitational constant [km^3/s^2]
const double GLONASS_SUN_SEMI_MAJOR_AXIS = 1.49598e8; //!< Semi-major axis of solar orbit [km];
const double GLONASS_SUN_ECCENTRICITY = 0.016719; //!< Eccentricity of solar orbit
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
// carrier and code frequencies
Adding RTCM Data Fields for GLONASS processing Adds GLONASS related data fields (DFxxx) for RTCM messages including MS1020, MS1087 and general MSM message types
2017-08-08 20:02:59 +00:00
const double GLONASS_L2_FREQ_HZ = FREQ2_GLO; //!< L1 [Hz]
Merge in GLONASS acquisition and tracking code
2017-08-29 23:32:34 +00:00
const double GLONASS_L1_CA_FREQ_HZ = FREQ1_GLO; //!< L1 [Hz]
const double GLONASS_L1_CA_DFREQ_HZ = DFRQ1_GLO; //!< Freq Bias for GLONASS L1 [Hz]
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
const double GLONASS_L1_CA_CODE_RATE_HZ = 0.511e6; //!< GLONASS L1 C/A code rate [chips/s]
const double GLONASS_L1_CA_CODE_LENGTH_CHIPS = 511.0; //!< GLONASS L1 C/A code length [chips]
const double GLONASS_L1_CA_CODE_PERIOD = 0.001; //!< GLONASS L1 C/A code period [seconds]
const double GLONASS_L1_CA_CHIP_PERIOD = 1.9569e-06; //!< GLONASS L1 C/A chip period [seconds]
Adding code for telemetry decoder algorithms
2017-07-10 06:00:49 +00:00
const double GLONASS_L1_CA_SYMBOL_RATE_BPS = 1000;
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
Adding proper TOW computation for GLONASS processing
2017-08-31 04:44:03 +00:00
//FIXME Probably should use leap seconds definitions of rtklib
const double GLONASS_LEAP_SECONDS[21][7] = { /* leap seconds (y,m,d,h,m,s,utc-gpst) */
{2019, 1, 1, 0, 0, 0, -20},
{2018, 1, 1, 0, 0, 0, -19},
{2017, 1, 1, 0, 0, 0, -18},
{2015, 7, 1, 0, 0, 0, -17},
{2012, 7, 1, 0, 0, 0, -16},
{2009, 1, 1, 0, 0, 0, -15},
{2006, 1, 1, 0, 0, 0, -14},
{1999, 1, 1, 0, 0, 0, -13},
{1997, 7, 1, 0, 0, 0, -12},
{1996, 1, 1, 0, 0, 0, -11},
{1994, 7, 1, 0, 0, 0, -10},
{1993, 7, 1, 0, 0, 0, -9},
{1992, 7, 1, 0, 0, 0, -8},
{1991, 1, 1, 0, 0, 0, -7},
{1990, 1, 1, 0, 0, 0, -6},
{1988, 1, 1, 0, 0, 0, -5},
{1985, 7, 1, 0, 0, 0, -4},
{1983, 7, 1, 0, 0, 0, -3},
{1982, 7, 1, 0, 0, 0, -2},
{1981, 7, 1, 0, 0, 0, -1},
{}
};
merging: Starts merge procedure for glonass branch from upstream Starts merging process of the acquisition and tracking code for GLONASS processing developed by Gabriel Araujo. Fixes compile warnings and errors introduced during rebase operation
2017-08-29 07:20:38 +00:00
// GLONASS SV's orbital slots PRN = (orbital_slot - 1)
const std::map<unsigned int, int> GLONASS_PRN =
{{ 0, 8,}, //For test
{ 1, 1,}, //Plane 1
{ 2,-4,}, //Plane 1
{ 3, 5,}, //Plane 1
{ 4, 6,}, //Plane 1
{ 5, 1,}, //Plane 1
{ 6,-4,}, //Plane 1
{ 7, 5,}, //Plane 1
{ 8, 6,}, //Plane 1
{ 9,-2,}, //Plane 2
{10,-7,}, //Plane 2
{11, 0,}, //Plane 2
{12,-1,}, //Plane 2
{13,-2,}, //Plane 2
{14,-7,}, //Plane 2
{15, 0,}, //Plane 2
{16,-1,}, //Plane 2
{17, 4,}, //Plane 3
{18,-3,}, //Plane 3
{19, 3,}, //Plane 3
{20, 2,}, //Plane 3
{21, 4,}, //Plane 3
{22,-3,}, //Plane 3
{23, 3,}, //Plane 3
{24, 2}}; //Plane 3
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
const double GLONASS_STARTOFFSET_ms = 68.802; //[ms] Initial sign. travel time (this cannot go here)
// OBSERVABLE HISTORY DEEP FOR INTERPOLATION
const int GLONASS_L1_CA_HISTORY_DEEP = 100;
// NAVIGATION MESSAGE DEMODULATION AND DECODING
bug_fix: Fixes bugs in telemetry decoding interface Fixes several bugs with the telemetry decoder interface and clean up the code with unused methods and members of the ephemeris object
2017-08-23 22:16:07 +00:00
#define GLONASS_GNAV_PREAMBLE {1, 1, 1, 1, 1, 0, 0, 0, 1, 1, 0, 1, 1, 1, 0, 1, 0, 1, 0, 0, 0, 0, 1, 0, 0, 1, 0, 1, 1, 0}
Merge in GLONASS acquisition and tracking code
2017-08-29 23:32:34 +00:00
const double GLONASS_GNAV_PREAMBLE_DURATION_S = 0.3;
bug_fix: Fixes bugs in telemetry decoding interface Fixes several bugs with the telemetry decoder interface and clean up the code with unused methods and members of the ephemeris object
2017-08-23 22:16:07 +00:00
const int GLONASS_GNAV_PREAMBLE_LENGTH_BITS = 30;
const int GLONASS_GNAV_PREAMBLE_LENGTH_SYMBOLS = 300;
Merge in GLONASS acquisition and tracking code
2017-08-29 23:32:34 +00:00
const int GLONASS_GNAV_PREAMBLE_PERIOD_SYMBOLS = 1700;
bug_fix: Fixes bugs in telemetry decoding interface Fixes several bugs with the telemetry decoder interface and clean up the code with unused methods and members of the ephemeris object
2017-08-23 22:16:07 +00:00
const int GLONASS_GNAV_TELEMETRY_RATE_BITS_SECOND = 50; //!< NAV message bit rate [bits/s]
const int GLONASS_GNAV_TELEMETRY_SYMBOLS_PER_BIT = 10;
const int GLONASS_GNAV_TELEMETRY_SYMBOLS_PER_PREAMBLE_BIT = 10;
const int GLONASS_GNAV_TELEMETRY_RATE_SYMBOLS_SECOND = GLONASS_GNAV_TELEMETRY_RATE_BITS_SECOND*GLONASS_GNAV_TELEMETRY_SYMBOLS_PER_BIT; //!< NAV message bit rate [symbols/s]
Merge in GLONASS acquisition and tracking code
2017-08-29 23:32:34 +00:00
const int GLONASS_GNAV_STRING_SYMBOLS = 2000; //!< Number of bits per string in the GNAV message (85 data bits + 30 time mark bits) [bits]
const int GLONASS_GNAV_STRING_BITS = 85; //!< Number of bits per string in the GNAV message (85 data bits + 30 time mark bits) [bits]
const int GLONASS_GNAV_HAMMING_CODE_BITS = 8; //!< Number of bits in hamming code sequence of GNAV message
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
writing code for crc computation in GLONASS processing
2017-07-07 06:02:50 +00:00
const std::vector<int> GLONASS_GNAV_CRC_I_INDEX {9, 10, 12, 13, 15, 17, 19, 20, 22, 24, 26, 28, 30, 32, 34, 35, 37, 39, 41, 43, 45, 47, 49, 51, 53, 55, 57, 59, 61, 63, 65, 66, 68, 70, 72, 74, 76, 78, 80, 82, 84};
const std::vector<int> GLONASS_GNAV_CRC_J_INDEX {9, 11, 12, 14, 15, 18, 19, 21, 22, 25, 26, 29, 30, 33, 34, 36, 37, 40, 41, 44, 45, 48, 49, 52, 53, 56, 57, 60, 61, 64, 65, 67, 68, 71, 72, 75, 76, 79, 80, 83, 84};
Fixing compilation warnings
2017-07-12 14:35:57 +00:00
const std::vector<int> GLONASS_GNAV_CRC_K_INDEX {10, 11, 12, 16, 17, 18, 19, 23, 24, 25, 26, 31, 32, 33, 34, 38, 39, 40, 41, 46, 47, 48, 49, 54, 55, 56, 57, 62, 63, 64, 65, 69, 70, 71, 72, 77, 78, 79, 80, 85};
writing code for crc computation in GLONASS processing
2017-07-07 06:02:50 +00:00
const std::vector<int> GLONASS_GNAV_CRC_L_INDEX {9, 11, 12, 14, 15, 18, 19, 21, 22, 25, 26, 29, 30, 33, 34, 36, 37, 40, 41, 44, 45, 48, 49, 52, 53, 56, 57, 60, 61, 64, 65, 67, 68, 71, 72, 75, 76, 79, 80, 83, 84};
const std::vector<int> GLONASS_GNAV_CRC_M_INDEX {20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 34, 50, 51, 52, 53, 54, 55, 56, 57, 58, 59, 60, 61, 62, 63, 64, 65, 81, 82, 83, 84, 85};
const std::vector<int> GLONASS_GNAV_CRC_N_INDEX {35, 36, 37, 38, 39, 40, 41, 42, 43, 44, 45, 46, 47, 48, 49, 50, 51, 52, 53, 54, 55, 56, 57, 58, 59, 60, 61, 62, 63, 64, 65, 66, 67, 68, 69, 70, 71, 72, 73, 74, 75, 76, 77, 78, 79, 80, 81, 82, 83, 84, 85};
const std::vector<int> GLONASS_GNAV_CRC_P_INDEX {66, 67, 68, 69, 70, 71, 72, 73, 74, 75, 76, 77, 78, 79, 80, 81, 82, 83, 84, 85};
const std::vector<int> GLONASS_GNAV_CRC_Q_INDEX {9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 34, 35, 36, 37, 38, 39, 40, 41, 42, 43, 44, 45, 46, 47, 48, 49, 50, 51, 52, 53, 54, 55, 56, 57, 58, 59, 60, 61, 62, 63, 64, 65, 66, 67, 68, 69, 70, 71, 72, 73, 74, 75, 76, 77, 78, 79, 80, 81, 82, 83, 84, 85};
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
// GLONASS GNAV NAVIGATION MESSAGE STRUCTURE
// NAVIGATION MESSAGE FIELDS POSITIONS (from IS-GPS-200E Appendix II)
// FRAME 1-4
// COMMON FIELDS
const std::vector<std::pair<int,int>> STRING_ID({{2,4}});
const std::vector<std::pair<int,int>> KX({{78,8}});
//STRING 1
const std::vector<std::pair<int,int>> P1({{8,2}});
bugfix: Fixing bugs with RINEX support Fixes compilation errors. Modifies GLONASS GNAV Ephemeris object to contain fields relative to GPS time using the boost posix time object. Adds unit tests to check existent and recently added code
2017-07-24 05:57:54 +00:00
const std::vector<std::pair<int,int>> T_K_HR({{10,5}});
unit-test: Adds and fixes unit test for system-parameters block Adding unit test for system-parameters block, testing string decoding logic for GLONASS GNAV messages. Bug fixes the code after several errors were detected while debugging
2017-08-19 21:04:14 +00:00
const std::vector<std::pair<int,int>> T_K_MIN({{15,6}});
const std::vector<std::pair<int,int>> T_K_SEC({{21,1}});
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
const std::vector<std::pair<int,int>> X_N_DOT ({{22,24}});
const std::vector<std::pair<int,int>> X_N_DOT_DOT ({{46,5}});
const std::vector<std::pair<int,int>> X_N({{51,27}});
//STRING 2
const std::vector<std::pair<int,int>> B_N({{6,3}});
const std::vector<std::pair<int,int>> P2({{9,1}});
const std::vector<std::pair<int,int>> T_B({{10,7}});
const std::vector<std::pair<int,int>> Y_N_DOT ({{22,24}});
const std::vector<std::pair<int,int>> Y_N_DOT_DOT ({{46,5}});
const std::vector<std::pair<int,int>> Y_N({{51,27}});
//STRING 3
const std::vector<std::pair<int,int>> P3({{6,1}});
const std::vector<std::pair<int,int>> GAMMA_N({{7,11}});
const std::vector<std::pair<int,int>> P({{19,2}});
gnav: Adding GLONASS GNAV Navigation Message Operations Adding code for navigation message computation for GLONASS GNAV code. Continues to fix the almanac position computation and fixes bugs in code due to compilation errors, coding style and Doxygen documentation
2017-06-21 04:44:44 +00:00
const std::vector<std::pair<int,int>> EPH_L_N({{21,1}});
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
const std::vector<std::pair<int,int>> Z_N_DOT ({{22,24}});
const std::vector<std::pair<int,int>> Z_N_DOT_DOT ({{46,5}});
const std::vector<std::pair<int,int>> Z_N({{51,27}});
// STRING 4
const std::vector<std::pair<int,int>> TAU_N({{6,22}});
const std::vector<std::pair<int,int>> DELTA_TAU_N({{28,5}});
const std::vector<std::pair<int,int>> E_N({{33,5}});
const std::vector<std::pair<int,int>> P4 ({{52,1}});
const std::vector<std::pair<int,int>> F_T ({{53,4}});
const std::vector<std::pair<int,int>> N_T({{60,11}});
const std::vector<std::pair<int,int>> N({{71,5}});
const std::vector<std::pair<int,int>> M({{76,2}});
// STRING 5
const std::vector<std::pair<int,int>> N_A({{6,11}});
const std::vector<std::pair<int,int>> TAU_C({{17,32}});
const std::vector<std::pair<int,int>> N_4({{50,5}});
const std::vector<std::pair<int,int>> TAU_GPS({{55,22}});
gnav: Adding GLONASS GNAV Navigation Message Operations Adding code for navigation message computation for GLONASS GNAV code. Continues to fix the almanac position computation and fixes bugs in code due to compilation errors, coding style and Doxygen documentation
2017-06-21 04:44:44 +00:00
const std::vector<std::pair<int,int>> ALM_L_N({{77,1}});
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
// STRING 6, 8, 10, 12, 14
const std::vector<std::pair<int,int>> C_N({{6,1}});
const std::vector<std::pair<int,int>> M_N_A({{7,2}});
const std::vector<std::pair<int,int>> n_A({{9,5}});
const std::vector<std::pair<int,int>> TAU_N_A({{14,10}});
const std::vector<std::pair<int,int>> LAMBDA_N_A({{24,21}});
const std::vector<std::pair<int,int>> DELTA_I_N_A({{45,18}});
const std::vector<std::pair<int,int>> EPSILON_N_A({{63,15}});
//STRING 7, 9, 11, 13, 15
const std::vector<std::pair<int,int>> OMEGA_N_A({{6,16}});
const std::vector<std::pair<int,int>> T_LAMBDA_N_A({{22,21}});
const std::vector<std::pair<int,int>> DELTA_T_N_A({{43,22}});
const std::vector<std::pair<int,int>> DELTA_T_DOT_N_A({{65,7}});
const std::vector<std::pair<int,int>> H_N_A({{72,5}});
Fixing compile warnings and adding work on unit test
2017-07-12 20:11:53 +00:00
// STRING 14 FRAME 5
const std::vector<std::pair<int,int>> B1({{6,11}});
const std::vector<std::pair<int,int>> B2({{17,10}});
gnav: Adding GLONASS GNAV Ephemeris, Almanac and UTC Model Generates code for GLONASS GNAV Ephemeris, Almanac and UTC Model with their respective decoding position indexes for string decoding and message parsing. Starts developing of satellite position computation based on its ephemeris and almanac information
2017-06-06 14:27:48 +00:00
#endif /* GNSS_SDR_GLONASS_L1_CA_H_ */
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