GPS/QZS CNAV/CNAV-2 or BDS CNAV-1/CNAV-2/CNAV-3 ephemeris. More...

Detailed Description

GPS/QZS CNAV/CNAV-2 or BDS CNAV-1/CNAV-2/CNAV-3 ephemeris.

Inheritance diagram for Ceph:

Collaboration diagram for Ceph:

Data Fields
E_NavMsgType	type = E_NavMsgType::NONE
	message type

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

SatSys	Sat
	satellite number

int	iode = -1
	BDS CNAV1/CNV2 IODE.

int	iodc = -1
	BDS CNAV1/CNV2 IODC.

E_Svh	svh
	SV health.

int	wnop = 0
	GPS/QZS: GPS week number (of prediction?) with AR.

int	flag = 0
	BDS B1C/B2a+B1C/B2b integrity flags.

GTime	toc = {}
	time of clock

GTime	toe = {}
	time of ephemeris, for GPS/QZS, TOE==TOC

GTime	top = {}
	time of prediction

GTime	ttm = {}
	transmission time

double	ura [4]
	user range accuracy GPS/QZS: 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 sis[0]=SISAI_oe, sis[1]=SISAI_ocb, sis[2]=SISAI_oc1, sis[3]=SISAI_oc2, sis[4]=SISMAI

double	tops = 0
	t_op (s) in week

double	toes = 0
	TOE (s) in week.

double	f0 = 0
	SV clock parameter (af0)

double	f1 = 0
	SV clock parameter (af1)

double	f2 = 0
	SV clock parameter (af2)

double	tgd [4] = {}
	group delay parameters GPS/QZS: tgd[0]=TGD BDS CNAV1/CNV2: tgd[0]=TGD_B1Cp, tgd[1]=TGD_B2ap BDS CNAV3: tgd[2]=TGD_B2bI

double	ttms = 0
	transmission time (s) within week

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

Field Documentation

◆ f0

double Ceph::f0 = 0

SV clock parameter (af0)

◆ f1

double Ceph::f1 = 0

SV clock parameter (af1)

◆ f2

double Ceph::f2 = 0

SV clock parameter (af2)

◆ flag

int Ceph::flag = 0

BDS B1C/B2a+B1C/B2b integrity flags.

◆ iodc

int Ceph::iodc = -1

BDS CNAV1/CNV2 IODC.

◆ iode

int Ceph::iode = -1

BDS CNAV1/CNV2 IODE.

◆ isc

double Ceph::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 Ceph::orb = E_SatType::NONE

BDS sat/orbit type.

◆ Sat

SatSys Ceph::Sat

satellite number

◆ sis

double Ceph::sis[5] = {}

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

◆ svh

E_Svh Ceph::svh

SV health.

◆ tgd

double Ceph::tgd[4] = {}

group delay parameters GPS/QZS: tgd[0]=TGD BDS CNAV1/CNV2: tgd[0]=TGD_B1Cp, tgd[1]=TGD_B2ap BDS CNAV3: tgd[2]=TGD_B2bI

◆ toc

GTime Ceph::toc = {}

time of clock

◆ toe

GTime Ceph::toe = {}

time of ephemeris, for GPS/QZS, TOE==TOC

◆ toes

double Ceph::toes = 0

TOE (s) in week.

◆ top

GTime Ceph::top = {}

time of prediction

◆ tops

double Ceph::tops = 0

t_op (s) in week

◆ ttm

GTime Ceph::ttm = {}

transmission time

◆ ttms

double Ceph::ttms = 0

transmission time (s) within week

◆ type

E_NavMsgType Ceph::type = E_NavMsgType::NONE

message type

◆ ura

double Ceph::ura[4]

Initial value:

=

{}

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

◆ wnop

int Ceph::wnop = 0

GPS/QZS: GPS week number (of prediction?) with AR.

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

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