GNSS-SDR  0.0.19
An Open Source GNSS Software Defined Receiver
galileo_reduced_ced.h
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1 /*!
2  * \file galileo_reduced_ced.h
3  * \brief Galileo Reduced Clock and Ephemeris Data storage class
4  * \author Carles Fernandez, 2021. cfernandez(at)cttc.cat
5  *
6  * -----------------------------------------------------------------------------
7  *
8  * GNSS-SDR is a Global Navigation Satellite System software-defined receiver.
9  * This file is part of GNSS-SDR.
10  *
11  * Copyright (C) 2010-2021 (see AUTHORS file for a list of contributors)
12  * SPDX-License-Identifier: GPL-3.0-or-later
13  *
14  * -----------------------------------------------------------------------------
15  */
16 
17 
18 #ifndef GNSS_SDR_GALILEO_REDUCED_CED_H
19 #define GNSS_SDR_GALILEO_REDUCED_CED_H
20 
21 #include "galileo_ephemeris.h"
22 #include <cstdint>
23 
24 /** \addtogroup Core
25  * \{ */
26 /** \addtogroup System_Parameters
27  * \{ */
28 
29 
30 /*!
31  * \brief This class manages the Galileo Reduced Clock and Ephemeris Data
32  */
34 {
35 public:
36  /*!
37  * Default constructor
38  */
39  Galileo_Reduced_CED() = default;
40 
41  /*!
42  * Convert to Galileo_Ephemeris
43  */
45 
46  uint32_t PRN{}; //!< Satellite ID
47  int32_t TOTRedCED{}; //!< Start time of transmission of the Reduced CED word in GST
48  int32_t IODnav{}; //!< Issue of Data
49  double DeltaAred{}; //!< Difference between the Reduced CED semi-major axis and the nominal semi-major axis [meters]
50  double exred{}; //!< Reduced CED eccentricity vector component x
51  double eyred{}; //!< Reduced CED eccentricity vector component y
52  double Deltai0red{}; //!< Difference between the Reduced CED inclination angle at reference time and the nominal inclination [rad]
53  double Omega0red{}; //!< Reduced CED longitude of ascending node at weekly epoch [rad]
54  double lambda0red{}; //!< Reduced CED mean argument of latitude [rad]
55  double af0red{}; //!< Reduced CED satellite clock bias correction coefficient [seconds]
56  double af1red{}; //!< Reduced CED satellite clock drift correction coefficient [seconds/seconds]
57 };
58 
59 
60 /** \} */
61 /** \} */
62 #endif // GNSS_SDR_GALILEO_REDUCED_CED_H
Galileo_Ephemeris compute_eph() const
double DeltaAred
Difference between the Reduced CED semi-major axis and the nominal semi-major axis [meters]...
double exred
Reduced CED eccentricity vector component x.
double Deltai0red
Difference between the Reduced CED inclination angle at reference time and the nominal inclination [r...
double af0red
Reduced CED satellite clock bias correction coefficient [seconds].
int32_t TOTRedCED
Start time of transmission of the Reduced CED word in GST.
Galileo_Reduced_CED()=default
double Omega0red
Reduced CED longitude of ascending node at weekly epoch [rad].
double af1red
Reduced CED satellite clock drift correction coefficient [seconds/seconds].
This class is a storage and orbital model functions for the Galileo SV ephemeris data as described in...
int32_t IODnav
Issue of Data.
uint32_t PRN
Satellite ID.
double lambda0red
Reduced CED mean argument of latitude [rad].
Interface of a Galileo EPHEMERIS storage.
This class manages the Galileo Reduced Clock and Ephemeris Data.
double eyred
Reduced CED eccentricity vector component y.