SBAS ephemeris. More...

Detailed Description

SBAS ephemeris.

Inheritance diagram for Seph:

Collaboration diagram for Seph:

Data Fields
E_NavMsgType	type = E_NavMsgType::NONE
	message type

SatSys	Sat
	satellite number

GTime	t0
	reference epoch time (GPST)

GTime	tof
	time of message frame (GPST)

int	sva
	SV accuracy (URA index)

double	ura
	SV accuracy in meters.

E_Svh	svh
	SV health.

VectorEcef	pos
	satellite position (m) (ecef)

VectorEcef	vel
	satellite velocity (m/s) (ecef)

VectorEcef	acc
	satellite acceleration (m/s^2) (ecef)

double	af0 = 0
	satellite clock-offset/drift (s)

double	af1 = 0
	satellite clock-drift (s/s)

int	iode = -1

GTime	toe

double	tofs
	TOF (s) within the week.

Field Documentation

◆ acc

VectorEcef Seph::acc

satellite acceleration (m/s^2) (ecef)

◆ af0

double Seph::af0 = 0

satellite clock-offset/drift (s)

◆ af1

double Seph::af1 = 0

satellite clock-drift (s/s)

◆ iode

int Seph::iode = -1

◆ pos

VectorEcef Seph::pos

satellite position (m) (ecef)

◆ Sat

SatSys Seph::Sat

satellite number

◆ sva

int Seph::sva

SV accuracy (URA index)

◆ svh

E_Svh Seph::svh

SV health.

◆ t0

GTime Seph::t0

reference epoch time (GPST)

◆ toe

GTime Seph::toe

◆ tof

GTime Seph::tof

time of message frame (GPST)

◆ tofs

double Seph::tofs

TOF (s) within the week.

◆ type

E_NavMsgType Seph::type = E_NavMsgType::NONE

message type

◆ ura

double Seph::ura

SV accuracy in meters.

◆ vel

VectorEcef Seph::vel

satellite velocity (m/s) (ecef)

The documentation for this struct was generated from the following file:

/ginan/src/cpp/common/ephemeris.hpp