GNSS-SDR  0.0.19
An Open Source GNSS Software Defined Receiver
glonass_gnav_almanac.h
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1 /*!
2  * \file glonass_gnav_almanac.h
3  * \brief Interface of a GLONASS GNAV ALMANAC storage
4  * \note Code added as part of GSoC 2017 program
5  * \author Damian Miralles, 2017. dmiralles2009(at)gmail.com
6  * \see <a href="http://russianspacesystems.ru/wp-content/uploads/2016/08/ICD_GLONASS_eng_v5.1.pdf">GLONASS ICD</a>
7  *
8  * -----------------------------------------------------------------------------
9  *
10  * GNSS-SDR is a Global Navigation Satellite System software-defined receiver.
11  * This file is part of GNSS-SDR.
12  *
13  * Copyright (C) 2010-2020 (see AUTHORS file for a list of contributors)
14  * SPDX-License-Identifier: GPL-3.0-or-later
15  *
16  * -----------------------------------------------------------------------------
17  */
18 
19 
20 #ifndef GNSS_SDR_GLONASS_ALMANAC_H
21 #define GNSS_SDR_GLONASS_ALMANAC_H
22 
23 #include <boost/serialization/nvp.hpp>
24 #include <cstdint>
25 
26 /** \addtogroup Core
27  * \{ */
28 /** \addtogroup System_Parameters
29  * \{ */
30 
31 
32 /*!
33  * \brief This class is a storage for the GLONASS SV ALMANAC data as described GLONASS ICD (Edition 5.1)
34  * \note Code added as part of GSoC 2017 program
35  * \see <a href="http://russianspacesystems.ru/wp-content/uploads/2016/08/ICD_GLONASS_eng_v5.1.pdf">GLONASS ICD</a>
36  */
38 {
39 public:
40  /*!
41  * Default constructor
42  */
43  Glonass_Gnav_Almanac() = default;
44 
45  double d_n_A{}; //!< Conventional number of satellite within GLONASS space segment [dimensionless]
46  double d_H_n_A{}; //!< Carrier frequency number of navigation RF signal transmitted by d_nA satellite as table 4.10 (0-31) [dimensionless]
47  double d_lambda_n_A{}; //!< Longitude of the first (within the d_NA day) ascending node of d_nA [radians]
48  double d_t_lambda_n_A{}; //!< Time of first ascending node passage [s]
49  double d_Delta_i_n_A{}; //!< Correction of the mean value of inclination of d_n_A satellite at instant t_lambda_n_A [radians]
50  double d_Delta_T_n_A{}; //!< Correction to the mean value of Draconian period of d_n_A satellite at instant t_lambda_n_A [s / orbital period]
51  double d_Delta_T_n_A_dot{}; //!< Rate of change of Draconian period of d_n_A satellite at instant t_lambda_n_A [s / orbital period^2]
52  double d_epsilon_n_A{}; //!< Eccentricity of d_n_A satellite at instant t_lambda_n_A [dimensionless]
53  double d_omega_n_A{}; //!< Argument of perigee of d_n_A satellite at instant t_lambdan_A [radians]
54  double d_M_n_A{}; //!< Type of satellite n_A [dimensionless]
55  double d_KP{}; //!< Notification on forthcoming leap second correction of UTC [dimensionless]
56  double d_tau_n_A{}; //!< Coarse value of d_n_A satellite time correction to GLONASS time at instant t_lambdan_A[s]
57  bool d_C_n{}; //!< Generalized “unhealthy flag” of n_A satellite at instant of almanac upload [dimensionless]
58  bool d_l_n{}; //!< Health flag for nth satellite; ln = 0 indicates the n-th satellite is helthy, ln = 1 indicates malfunction of this nth satellite [dimensionless]
59 
60  // Satellite Identification Information
61  int32_t i_satellite_freq_channel{}; //!< SV Frequency Channel Number
62  uint32_t PRN{}; //!< SV PRN Number, equivalent to slot number for compatibility with GPS
63  uint32_t i_satellite_slot_number{}; //!< SV Slot Number
64 
65  template <class Archive>
66  /*!
67  * \brief Serialize is a boost standard method to be called by the boost XML
68  * serialization. Here is used to save the almanac data on disk file.
69  */
70  void serialize(Archive& archive, const uint32_t version)
71  {
72  if (version)
73  {
74  };
75 
76  archive& BOOST_SERIALIZATION_NVP(i_satellite_freq_channel);
77  archive& BOOST_SERIALIZATION_NVP(PRN);
78  archive& BOOST_SERIALIZATION_NVP(i_satellite_slot_number);
79  archive& BOOST_SERIALIZATION_NVP(d_n_A);
80  archive& BOOST_SERIALIZATION_NVP(d_H_n_A);
81  archive& BOOST_SERIALIZATION_NVP(d_lambda_n_A);
82  archive& BOOST_SERIALIZATION_NVP(d_t_lambda_n_A);
83  archive& BOOST_SERIALIZATION_NVP(d_Delta_i_n_A);
84  archive& BOOST_SERIALIZATION_NVP(d_Delta_T_n_A);
85  archive& BOOST_SERIALIZATION_NVP(d_Delta_T_n_A_dot);
86  archive& BOOST_SERIALIZATION_NVP(d_epsilon_n_A);
87  archive& BOOST_SERIALIZATION_NVP(d_omega_n_A);
88  archive& BOOST_SERIALIZATION_NVP(d_M_n_A);
89  archive& BOOST_SERIALIZATION_NVP(d_KP);
90  archive& BOOST_SERIALIZATION_NVP(d_tau_n_A);
91  archive& BOOST_SERIALIZATION_NVP(d_C_n);
92  archive& BOOST_SERIALIZATION_NVP(d_l_n);
93  }
94 };
95 
96 
97 /** \} */
98 /** \} */
99 #endif // GNSS_SDR_GLONASS_ALMANAC_H
double d_omega_n_A
Argument of perigee of d_n_A satellite at instant t_lambdan_A [radians].
double d_Delta_T_n_A
Correction to the mean value of Draconian period of d_n_A satellite at instant t_lambda_n_A [s / orbi...
void serialize(Archive &archive, const uint32_t version)
Serialize is a boost standard method to be called by the boost XML serialization. Here is used to sav...
Glonass_Gnav_Almanac()=default
double d_n_A
Conventional number of satellite within GLONASS space segment [dimensionless].
double d_M_n_A
Type of satellite n_A [dimensionless].
bool d_l_n
Health flag for nth satellite; ln = 0 indicates the n-th satellite is helthy, ln = 1 indicates malfun...
double d_tau_n_A
Coarse value of d_n_A satellite time correction to GLONASS time at instant t_lambdan_A[s].
double d_KP
Notification on forthcoming leap second correction of UTC [dimensionless].
int32_t i_satellite_freq_channel
SV Frequency Channel Number.
bool d_C_n
Generalized “unhealthy flag” of n_A satellite at instant of almanac upload [dimensionless].
double d_epsilon_n_A
Eccentricity of d_n_A satellite at instant t_lambda_n_A [dimensionless].
double d_lambda_n_A
Longitude of the first (within the d_NA day) ascending node of d_nA [radians].
This class is a storage for the GLONASS SV ALMANAC data as described GLONASS ICD (Edition 5...
double d_Delta_i_n_A
Correction of the mean value of inclination of d_n_A satellite at instant t_lambda_n_A [radians]...
uint32_t PRN
SV PRN Number, equivalent to slot number for compatibility with GPS.
uint32_t i_satellite_slot_number
SV Slot Number.
double d_H_n_A
Carrier frequency number of navigation RF signal transmitted by d_nA satellite as table 4...
double d_Delta_T_n_A_dot
Rate of change of Draconian period of d_n_A satellite at instant t_lambda_n_A [s / orbital period^2]...
double d_t_lambda_n_A
Time of first ascending node passage [s].