This class is a storage and orbital model functions for the Galileo SV ephemeris data as described in Galileo ICD paragraph 5.1.1. More...

#include <galileo_ephemeris.h>

Inheritance diagram for Galileo_Ephemeris:

Public Member Functions
double	Galileo_System_Time (double week_number, double TOW)
	Galileo System Time (GST), ICD paragraph 5.1.2. More...

template<class Archive >
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 save the ephemeris data on disk file. More...

Public Member Functions inherited from Gnss_Ephemeris
double	sv_clock_drift (double transmitTime)
	Sets (satClkDrift) and (dtr), and returns the clock drift in seconds according to the User Algorithm for SV Clock Correction (IS-GPS-200M, 20.3.3.3.3.1, and Galileo OS SIS ICD, 5.1.4). More...

double	predicted_doppler (double rx_time_s, double lat, double lon, double h, double ve, double vn, double vu, int band) const
	Computes prediction of the Doppler shift for a given time and receiver's position and velocity. \[ f_{d} = - \mathbf{v} \frac{\mathbf{x}^{T}}{\left\| \mathbf{x} \right\| } \frac{f_{L}}{c} \] where: \[ \mathbf{v} = \mathbf{v}_{sat} - \mathbf{v}_{rx} \] \[ \mathbf{x} = \mathbf{x}_{sat} - \mathbf{x}_{rx} \] \[ \left\| \mathbf{x} \right\| = \sqrt{\mathbf{x}\mathbf{x}^{T}} \] . More...

void	satellitePosition (double transmitTime)
	Computes the ECEF SV coordinates and ECEF velocity. More...

Public Attributes
int32_t	IOD_ephemeris {}

int32_t	IOD_nav {}

int32_t	SISA {}
	Signal in space accuracy index. More...

int32_t	E5a_HS {}
	E5a Signal Health Status. More...

int32_t	E5b_HS {}
	E5b Signal Health Status. More...

int32_t	E1B_HS {}
	E1B Signal Health Status. More...

bool	E5a_DVS {}
	E5a Data Validity Status. More...

bool	E5b_DVS {}
	E5b Data Validity Status. More...

bool	E1B_DVS {}
	E1B Data Validity Status. More...

double	BGD_E1E5a {}
	E1-E5a Broadcast Group Delay [s]. More...

double	BGD_E1E5b {}
	E1-E5b Broadcast Group Delay [s]. More...

bool	flag_all_ephemeris {}

Public Attributes inherited from Gnss_Ephemeris
uint32_t	PRN {}
	SV ID. More...

double	M_0 {}
	Mean anomaly at reference time [rad]. More...

double	delta_n {}
	Mean motion difference from computed value [rad/sec]. More...

double	ecc {}
	Eccentricity. More...

double	sqrtA {}
	Square root of the semi-major axis [meters^1/2]. More...

double	OMEGA_0 {}
	Longitude of ascending node of orbital plane at weekly epoch [rad]. More...

double	i_0 {}
	Inclination angle at reference time [rad]. More...

double	omega {}
	Argument of perigee [rad]. More...

double	OMEGAdot {}
	Rate of right ascension [rad/sec]. More...

double	idot {}
	Rate of inclination angle [rad/sec]. More...

double	Cuc {}
	Amplitude of the cosine harmonic correction term to the argument of latitude [rad]. More...

double	Cus {}
	Amplitude of the sine harmonic correction term to the argument of latitude [rad]. More...

double	Crc {}
	Amplitude of the cosine harmonic correction term to the orbit radius [meters]. More...

double	Crs {}
	Amplitude of the sine harmonic correction term to the orbit radius [meters]. More...

double	Cic {}
	Amplitude of the cosine harmonic correction term to the angle of inclination [rad]. More...

double	Cis {}
	Amplitude of the sine harmonic correction term to the angle of inclination [rad]. More...

int32_t	toe {}
	Ephemeris reference time [s]. More...

int32_t	toc {}
	Clock correction data reference Time of Week [sec]. More...

double	af0 {}
	SV clock bias correction coefficient [s]. More...

double	af1 {}
	SV clock drift correction coefficient [s/s]. More...

double	af2 {}
	SV clock drift rate correction coefficient [s/s^2]. More...

double	satClkDrift {}
	SV clock drift. More...

double	dtr {}
	Relativistic clock correction term. More...

int32_t	WN {}
	Week number. More...

int32_t	tow {}
	Time of Week. More...

double	satpos_X {}
	Earth-fixed coordinate x of the satellite [m]. Intersection of the IERS Reference Meridian (IRM) and the plane passing through the origin and normal to the Z-axis. More...

double	satpos_Y {}
	Earth-fixed coordinate y of the satellite [m]. Completes a right-handed, Earth-Centered, Earth-Fixed orthogonal coordinate system. More...

double	satpos_Z {}
	Earth-fixed coordinate z of the satellite [m]. The direction of the IERS (International Earth Rotation and Reference Systems Service) Reference Pole (IRP). More...

double	satvel_X {}
	Earth-fixed velocity coordinate x of the satellite [m]. More...

double	satvel_Y {}
	Earth-fixed velocity coordinate y of the satellite [m]. More...

double	satvel_Z {}
	Earth-fixed velocity coordinate z of the satellite [m]. More...

Additional Inherited Members
Protected Attributes inherited from Gnss_Ephemeris
char	System {}
	Character ID of the GNSS system. 'G': GPS. 'E': Galileo. 'B': BeiDou. More...