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Fix units of ephemeris angles in comments

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Fix angle units in retrieval of reduced CED ephemeris
This commit is contained in:
Carles Fernandez
2022-06-22 12:48:25 +02:00
parent d82acd9c41
commit 525a8ba602
8 changed files with 66 additions and 68 deletions
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22
docs/protobuf/galileo_ephemeris.proto
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@@ -6,21 +6,21 @@ package gnss_sdr;
message GalileoEphemeris {
int32 PRN = 1; // SV ID
double M_0 = 2; // Mean anomaly at reference time [semi-circles]
double delta_n = 3; // Mean motion difference from computed value [semi-circles/sec]
double M_0 = 2; // Mean anomaly at reference time [rad]
double delta_n = 3; // Mean motion difference from computed value [rad/sec]
double ecc = 4; // Eccentricity
double sqrtA = 5; // Square root of the semi-major axis [meters^1/2]
double OMEGA_0 = 6; // Longitude of ascending node of orbital plane at weekly epoch [semi-circles]
double i_0 = 7; // Inclination angle at reference time [semi-circles]
double omega = 8; // Argument of perigee [semi-circles]
double OMEGAdot = 9; // Rate of right ascension [semi-circles/sec]
double idot = 10; // Rate of inclination angle [semi-circles/sec]
double Cuc = 11; // Amplitude of the cosine harmonic correction term to the argument of latitude [radians]
double Cus = 12; // Amplitude of the sine harmonic correction term to the argument of latitude [radians]
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]
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]
double Cic = 15; // Amplitude of the cosine harmonic correction term to the angle of inclination [radians]
double Cis = 16; // Amplitude of the sine harmonic correction term to the angle of inclination [radians]
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]
int32 toe = 17; // Ephemeris reference time [s]
// Clock correction parameters

22
docs/protobuf/gps_ephemeris.proto
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@@ -6,21 +6,21 @@ package gnss_sdr;
message GpsEphemeris {
int32 PRN = 1; // SV ID
double M_0 = 2; // Mean anomaly at reference time [semi-circles]
double delta_n = 3; // Mean motion difference from computed value [semi-circles/sec]
double M_0 = 2; // Mean anomaly at reference time [rad]
double delta_n = 3; // Mean motion difference from computed value [rad/sec]
double ecc = 4; // Eccentricity
double sqrtA = 5; // Square root of the semi-major axis [meters^1/2]
double OMEGA_0 = 6; // Longitude of ascending node of orbital plane at weekly epoch [semi-circles]
double i_0 = 7; // Inclination angle at reference time [semi-circles]
double omega = 8; // Argument of perigee [semi-circles]
double OMEGAdot = 9; // Rate of right ascension [semi-circles/sec]
double idot = 10; // Rate of inclination angle [semi-circles/sec]
double Cuc = 11; // Amplitude of the cosine harmonic correction term to the argument of latitude [radians]
double Cus = 12; // Amplitude of the sine harmonic correction term to the argument of latitude [radians]
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]
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]
double Cic = 15; // Amplitude of the cosine harmonic correction term to the angle of inclination [radians]
double Cis = 16; // Amplitude of the sine harmonic correction term to the angle of inclination [radians]
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]
int32 toe = 17; // Ephemeris reference time [s]
// Clock correction parameters