GPS/QZS/GAL/BDS broadcast ephemeris. More...

Detailed Description

GPS/QZS/GAL/BDS broadcast ephemeris.

Inheritance diagram for Eph:

Collaboration diagram for Eph:

Public Member Functions
template<class ARCHIVE >
void	serialize (ARCHIVE &ar, const unsigned int &version)

Data Fields
E_NavMsgType	type = E_NavMsgType::NONE
	message type

SatSys	Sat
	satellite number

int	iode = -1
	GPS/QZS: IODE, GAL: IODnav.

int	iodc = 0
	IODC.

int	aode
	BDS AODE.

int	aodc
	BDS AODC.

int	sva
	SV accuracy (URA index)

E_Svh	svh
	SV health.

int	week
	GPS/QZS: gps week, GAL:gps week (i.e. galileo week + 1024), BDS: beidou week.

int	code = 0
	GPS/QZS: code on L2, GAL: data source.

int	flag = 0
	GPS L2 P data flag.

int	howTow
	Hand over word time.

GTime	toc
	time of clock

GTime	toe
	time of ephemeris

GTime	ttm
	transmission time

double	toes
	TOE (s) in week.

double	fit
	fit interval (h)

double	f0
	SV clock parameter (af0)

double	f1
	SV clock parameter (af1)

double	f2
	SV clock parameter (af2)

double	tgd [4] = {}
	group delay parameters GPS/QZS:tgd[0]=TGD GAL :tgd[0]=BGD E5a/E1,tgd[1]=BGD E5b/E1 BDS :tgd[0]=BGD1,tgd[1]=BGD2

E_SatType	orb = E_SatType::NONE
	BDS sat/orbit type.

GTime	top = {}
	time of prediction

double	tops = 0
	t_op (s) in week

double	ura [4] = {}
	user range accuracy or GAL SISA GPS/QZS CNVX: ura[0]=URAI_NED0, ura[1]=URAI_NED1, ura[2]=URAI_NED2, ura[3]=URAI_ED

double	isc [6] = {}
	inter-signal corrections GPS/QZS CNAV: isc[0]=ISC_L1CA, isc[1]=ISC_L2C, isc[2]=ISC_L5I5, isc[3]=ISC_L5Q5 GPS/QZS CNV2: isc[0]=ISC_L1CA, isc[1]=ISC_L2C, isc[2]=ISC_L5I5, isc[3]=ISC_L5Q5, isc[4]=ISC_L1Cd, isc[5]=ISC_L1Cp BDS CNV1: isc[0]=ISC_B1Cd BDS CNV2: isc[1]=ISC_B2ad

double	sis [5] = {}
	signal in space accuracy index BDS CNVX sis[0]=SISAI_oe, sis[1]=SISAI_ocb, sis[2]=SISAI_oc1, sis[3]=SISAI_oc2, sis[4]=SISMAI

double	tocs
	TOC (s) within week.

int	weekRollOver
	week number (rolled over)

double	sqrtA
	sqrt A

int	e5a_hs = 0
	GAL E5a signal health status.

int	e5a_dvs = 0
	GAL E5a data validity status.

int	e5b_hs = 0
	GAL E5b signal health status.

int	e5b_dvs = 0
	GAL E5b data validity status.

int	e1_hs = 0
	GAL E1 signal health status.

int	e1_dvs = 0
	GAL E1 data validity status.

double	ttms = 0
	transmission time (s) within week

int	fitFlag = 0
	fit flag

Data Fields inherited from KeplerEph
double	A = 0
	semi major axis

double	e = 0
	eccentricity

double	i0 = 0
	inclination

double	OMG0 = 0
	right ascension of ascending node

double	omg = 0
	argument of perigee

double	M0 = 0
	mean anomoly

double	deln = 0
	correction mean motion

double	OMGd = 0
	rate of OMG

double	idot = 0
	rate of inclination

double	crc = 0
	correction radial cosine

double	crs = 0
	correction radial sine

double	cuc = 0
	correction lattitude cosine

double	cus = 0
	correction lattitude sine

double	cic = 0
	correction inclination cosine

double	cis = 0
	correction inclination sine

double	dn0d = 0
	rate of correction mean motion

double	Adot = 0
	rate of A

Member Function Documentation

◆ serialize()

template<class ARCHIVE >

void Eph::serialize	(	ARCHIVE &	ar,
		const unsigned int &	version )

inline

Field Documentation

◆ aodc

int Eph::aodc

BDS AODC.

◆ aode

int Eph::aode

BDS AODE.

◆ code

int Eph::code = 0

GPS/QZS: code on L2, GAL: data source.

◆ e1_dvs

int Eph::e1_dvs = 0

GAL E1 data validity status.

◆ e1_hs

int Eph::e1_hs = 0

GAL E1 signal health status.

◆ e5a_dvs

int Eph::e5a_dvs = 0

GAL E5a data validity status.

◆ e5a_hs

int Eph::e5a_hs = 0

GAL E5a signal health status.

◆ e5b_dvs

int Eph::e5b_dvs = 0

GAL E5b data validity status.

◆ e5b_hs

int Eph::e5b_hs = 0

GAL E5b signal health status.

◆ fit

double Eph::fit

fit interval (h)

◆ fitFlag

int Eph::fitFlag = 0

fit flag

◆ flag

int Eph::flag = 0

GPS L2 P data flag.

◆ howTow

int Eph::howTow

Hand over word time.

◆ iodc

int Eph::iodc = 0

IODC.

◆ iode

int Eph::iode = -1

GPS/QZS: IODE, GAL: IODnav.

◆ isc

double Eph::isc[6] = {}

inter-signal corrections GPS/QZS CNAV: isc[0]=ISC_L1CA, isc[1]=ISC_L2C, isc[2]=ISC_L5I5, isc[3]=ISC_L5Q5 GPS/QZS CNV2: isc[0]=ISC_L1CA, isc[1]=ISC_L2C, isc[2]=ISC_L5I5, isc[3]=ISC_L5Q5, isc[4]=ISC_L1Cd, isc[5]=ISC_L1Cp BDS CNV1: isc[0]=ISC_B1Cd BDS CNV2: isc[1]=ISC_B2ad

◆ orb

E_SatType Eph::orb = E_SatType::NONE

BDS sat/orbit type.

◆ Sat

SatSys Eph::Sat

satellite number

◆ sis

double Eph::sis[5] = {}

signal in space accuracy index BDS CNVX sis[0]=SISAI_oe, sis[1]=SISAI_ocb, sis[2]=SISAI_oc1, sis[3]=SISAI_oc2, sis[4]=SISMAI

◆ sqrtA

double Eph::sqrtA

sqrt A

◆ sva

int Eph::sva

SV accuracy (URA index)

◆ svh

E_Svh Eph::svh

SV health.

◆ tgd

double Eph::tgd[4] = {}

group delay parameters GPS/QZS:tgd[0]=TGD GAL :tgd[0]=BGD E5a/E1,tgd[1]=BGD E5b/E1 BDS :tgd[0]=BGD1,tgd[1]=BGD2

◆ toc

GTime Eph::toc

time of clock

◆ tocs

double Eph::tocs

TOC (s) within week.

◆ toe

GTime Eph::toe

time of ephemeris

◆ toes

double Eph::toes

TOE (s) in week.

◆ top

GTime Eph::top = {}

time of prediction

◆ tops

double Eph::tops = 0

t_op (s) in week

◆ ttm

GTime Eph::ttm

transmission time

◆ ttms

double Eph::ttms = 0

transmission time (s) within week

◆ type

E_NavMsgType Eph::type = E_NavMsgType::NONE

message type

◆ ura

double Eph::ura[4] = {}

user range accuracy or GAL SISA GPS/QZS CNVX: ura[0]=URAI_NED0, ura[1]=URAI_NED1, ura[2]=URAI_NED2, ura[3]=URAI_ED

◆ week

int Eph::week

GPS/QZS: gps week, GAL:gps week (i.e. galileo week + 1024), BDS: beidou week.

◆ weekRollOver

int Eph::weekRollOver

week number (rolled over)

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

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