2021-02-22 12:42:54 +00:00
|
|
|
// SPDX-License-Identifier: BSD-3-Clause
|
|
|
|
// SPDX-FileCopyrightText: 2018-2021 Carles Fernandez-Prades <carles.fernandez@cttc.es>
|
|
|
|
syntax = "proto3";
|
|
|
|
|
|
|
|
package gnss_sdr;
|
|
|
|
|
|
|
|
message GalileoEphemeris {
|
|
|
|
int32 PRN = 1; // SV ID
|
2022-06-22 10:48:25 +00:00
|
|
|
double M_0 = 2; // Mean anomaly at reference time [rad]
|
|
|
|
double delta_n = 3; // Mean motion difference from computed value [rad/sec]
|
2021-02-22 12:42:54 +00:00
|
|
|
double ecc = 4; // Eccentricity
|
|
|
|
double sqrtA = 5; // Square root of the semi-major axis [meters^1/2]
|
2022-06-22 10:48:25 +00:00
|
|
|
double OMEGA_0 = 6; // Longitude of ascending node of orbital plane at weekly epoch [rad]
|
|
|
|
double i_0 = 7; // Inclination angle at reference time [rad]
|
|
|
|
double omega = 8; // Argument of perigee [rad]
|
|
|
|
double OMEGAdot = 9; // Rate of right ascension [rad/sec]
|
|
|
|
double idot = 10; // Rate of inclination angle [rad/sec]
|
|
|
|
double Cuc = 11; // Amplitude of the cosine harmonic correction term to the argument of latitude [rad]
|
|
|
|
double Cus = 12; // Amplitude of the sine harmonic correction term to the argument of latitude [rad]
|
2021-02-22 12:42:54 +00:00
|
|
|
double Crc = 13; // Amplitude of the cosine harmonic correction term to the orbit radius [meters]
|
|
|
|
double Crs = 14; // Amplitude of the sine harmonic correction term to the orbit radius [meters]
|
2022-06-22 10:48:25 +00:00
|
|
|
double Cic = 15; // Amplitude of the cosine harmonic correction term to the angle of inclination [rad]
|
|
|
|
double Cis = 16; // Amplitude of the sine harmonic correction term to the angle of inclination [rad]
|
2021-02-22 12:42:54 +00:00
|
|
|
int32 toe = 17; // Ephemeris reference time [s]
|
|
|
|
|
|
|
|
// Clock correction parameters
|
|
|
|
int32 toc = 18; // Clock correction data reference Time of Week [sec]
|
|
|
|
double af0 = 19; // SV clock bias correction coefficient [s]
|
|
|
|
double af1 = 20; // SV clock drift correction coefficient [s/s]
|
|
|
|
double af2 = 21; // SV clock drift rate correction coefficient [s/s^2]
|
|
|
|
|
|
|
|
double satClkDrift = 22; // SV clock drift
|
|
|
|
double dtr = 23; // Relativistic clock correction term
|
|
|
|
|
|
|
|
// Time
|
|
|
|
int32 WN = 24; // Week number
|
|
|
|
int32 tow = 25; // Time of Week
|
|
|
|
|
|
|
|
// Galileo-specific parameters
|
|
|
|
int32 IOD_ephemeris = 26;
|
|
|
|
int32 IOD_nav = 27;
|
|
|
|
|
|
|
|
// SV status
|
|
|
|
int32 SISA = 28; // Signal in space accuracy index
|
|
|
|
int32 E5a_HS = 29; // E5a Signal Health Status
|
|
|
|
int32 E5b_HS = 30; // E5b Signal Health Status
|
|
|
|
int32 E1B_HS = 31; // E1B Signal Health Status
|
|
|
|
bool E5a_DVS = 32; // E5a Data Validity Status
|
|
|
|
bool E5b_DVS = 33; // E5b Data Validity Status
|
|
|
|
bool E1B_DVS = 34; // E1B Data Validity Status
|
|
|
|
double BGD_E1E5a = 35; // E1-E5a Broadcast Group Delay [s]
|
|
|
|
double BGD_E1E5b = 36; // E1-E5b Broadcast Group Delay [s]
|
|
|
|
}
|