Merge branch 'next' of https://github.com/gnss-sdr/gnss-sdr into next

docs/protobuf/monitor_galileo_ephemeris.proto

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+// SPDX-License-Identifier: BSD-3-Clause
+// SPDX-FileCopyrightText: 2018-2020 Carles Fernandez-Prades <carles.fernandez@cttc.es>
+syntax = "proto3";
+
+package gnss_sdr;
+
+message MonitorGalileoEphemeris {
+    /* Galileo ephemeris are 16 parameters and here are reported following the ICD order, paragraph 5.1.1.
+       The number in the name after underscore (_1, _2, _3 and so on) refers to the page were we can find that parameter */
+    int32 IOD_ephemeris=1;
+    int32 IOD_nav_1=2;
+    double M0_1=3;            //!< Mean anomaly at reference time [semi-circles]
+    double delta_n_3=4;       //!< Mean motion difference from computed value [semi-circles/sec]
+    double e_1=5;             //!< Eccentricity
+    double A_1=6;             //!< Square root of the semi-major axis [meters^1/2]
+    double OMEGA_0_2=7;       //!< Longitude of ascending node of orbital plane at weekly epoch [semi-circles]
+    double i_0_2=8;           //!< Inclination angle at reference time  [semi-circles]
+    double omega_2=9;         //!< Argument of perigee [semi-circles]
+    double OMEGA_dot_3=10;     //!< Rate of right ascension [semi-circles/sec]
+    double iDot_2=11;          //!< Rate of inclination angle [semi-circles/sec]
+    double C_uc_3=12;          //!< Amplitude of the cosine harmonic correction term to the argument of latitude [radians]
+    double C_us_3=13;          //!< Amplitude of the sine harmonic correction term to the argument of latitude [radians]
+    double C_rc_3=14;          //!< Amplitude of the cosine harmonic correction term to the orbit radius [meters]
+    double C_rs_3=15;          //!< Amplitude of the sine harmonic correction term to the orbit radius [meters]
+    double C_ic_4=16;          //!< Amplitude of the cosine harmonic correction term to the angle of inclination [radians]
+    double C_is_4=17;          //!< Amplitude of the sine harmonic correction term to the angle of inclination [radians]
+    uint32 d_Toe=18;  // Ephemeris reference time
+
+    /*Clock correction parameters*/
+    uint32 d_Toc=19;  // Clock correction data reference Time of Week
+    double af0_4=20;           //!< SV clock bias correction coefficient [s]
+    double af1_4=21;           //!< SV clock drift correction coefficient [s/s]
+    double af2_4=22;           //!< SV clock drift rate correction coefficient [s/s^2]
+
+    /*GST*/
+    // Not belong to ephemeris set (page 1 to 4)
+    int32 WN_5=23;   //!< Week number
+    int32 TOW_5=24;  //!< Time of Week
+    double Galileo_satClkDrift=25;
+    double Galileo_dtr=26;  //!< relativistic clock correction term
+
+    // SV status
+    int32 SISA_3=27;
+    int32 E5a_HS=28;    //!< E5a Signal Health Status
+    int32 E5b_HS_5=29;  //!< E5b Signal Health Status
+    int32 E1B_HS_5=30;  //!< E1B Signal Health Status
+    bool E5a_DVS=31;      //!< E5a Data Validity Status
+    bool E5b_DVS_5=32;    //!< E5b Data Validity Status
+    bool E1B_DVS_5=33;    //!< E1B Data Validity Status
+
+    double BGD_E1E5a_5=34;  //!< E1-E5a Broadcast Group Delay [s]
+    double BGD_E1E5b_5=35;  //!< E1-E5b Broadcast Group Delay [s]
+    
+    int32 i_satellite_PRN=36; //!< SV PRN NUMBER
+}

docs/protobuf/monitor_gps_ephemeris.proto

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+// SPDX-License-Identifier: BSD-3-Clause
+// SPDX-FileCopyrightText: 2018-2020 Carles Fernandez-Prades <carles.fernandez@cttc.es>
+syntax = "proto3";
+
+package gnss_sdr;
+
+message MonitorGpsEphemeris {
+    uint32 i_satellite_PRN=1;  // SV PRN NUMBER
+    double d_TOW=2;             //!< Time of GPS Week of the ephemeris set (taken from subframes TOW) [s]
+    double d_Crs=3;             //!< Amplitude of the Sine Harmonic Correction Term to the Orbit Radius [m]
+    double d_Delta_n=4;         //!< Mean Motion Difference From Computed Value [semi-circles/s]
+    double d_M_0=5;             //!< Mean Anomaly at Reference Time [semi-circles]
+    double d_Cuc=6;             //!< Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude [rad]
+    double d_e_eccentricity=7;  //!< Eccentricity [dimensionless]
+    double d_Cus=8;             //!< Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude [rad]
+    double d_sqrt_A=9;          //!< Square Root of the Semi-Major Axis [sqrt(m)]
+    uint32 d_Toe=10;             //!< Ephemeris data reference time of week (Ref. 20.3.3.4.3 IS-GPS-200K) [s]
+    uint32 d_Toc=11;             //!< clock data reference time (Ref. 20.3.3.3.3.1 IS-GPS-200K) [s]
+    double d_Cic=12;           //!< Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination [rad]
+    double d_OMEGA0=13;        //!< Longitude of Ascending Node of Orbit Plane at Weekly Epoch [semi-circles]
+    double d_Cis=14;           //!< Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination [rad]
+    double d_i_0=15;           //!< Inclination Angle at Reference Time [semi-circles]
+    double d_Crc=16;           //!< Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius [m]
+    double d_OMEGA=17;         //!< Argument of Perigee [semi-cicles]
+    double d_OMEGA_DOT=18;     //!< Rate of Right Ascension [semi-circles/s]
+    double d_IDOT=19;          //!< Rate of Inclination Angle [semi-circles/s]
+    int32 i_code_on_L2=20;   //!< If 1, P code ON in L2;  if 2, C/A code ON in L2;
+    int32 i_GPS_week=21;     //!< GPS week number, aka WN [week]
+    bool b_L2_P_data_flag=22;  //!< When true, indicates that the NAV data stream was commanded OFF on the P-code of the L2 channel
+    int32 i_SV_accuracy=23;  //!< User Range Accuracy (URA) index of the SV (reference paragraph 6.2.1) for the standard positioning service user (Ref 20.3.3.3.1.3 IS-GPS-200K)
+    int32 i_SV_health=24;
+    double d_TGD=25;       //!< Estimated Group Delay Differential: L1-L2 correction term only for the benefit of "L1 P(Y)" or "L2 P(Y)" s users [s]
+    double d_IODC=26;      //!< Issue of Data, Clock
+    double d_IODE_SF2=27;  //!< Issue of Data, Ephemeris (IODE), subframe 2
+    double d_IODE_SF3=28;  //!< Issue of Data, Ephemeris(IODE), subframe 3
+    int32 i_AODO=29;     //!< Age of Data Offset (AODO) term for the navigation message correction table (NMCT) contained in subframe 4 (reference paragraph 20.3.3.5.1.9) [s]
+
+    bool b_fit_interval_flag=30;  //!< indicates the curve-fit interval used by the CS (Block II/IIA/IIR/IIR-M/IIF) and SS (Block IIIA) in determining the ephemeris parameters, as follows: 0 = 4 hours, 1 = greater than 4 hours.
+    double d_spare1=31;
+    double d_spare2=32;
+
+    double d_A_f0=33;  //!< Coefficient 0 of code phase offset model [s]
+    double d_A_f1=34;  //!< Coefficient 1 of code phase offset model [s/s]
+    double d_A_f2=35;  //!< Coefficient 2 of code phase offset model [s/s^2]
+    
+    bool b_integrity_status_flag=36;
+    bool b_alert_flag=37;         //!< If true, indicates  that the SV URA may be worse than indicated in d_SV_accuracy, use that SV at our own risk.
+    bool b_antispoofing_flag=38;  //!<  If true, the AntiSpoofing mode is ON in that SV
+}