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Ginan
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GPS/QZS CNAV/CNAV-2 or BDS CNAV-1/CNAV-2/CNAV-3 ephemeris. More...
GPS/QZS CNAV/CNAV-2 or BDS CNAV-1/CNAV-2/CNAV-3 ephemeris.
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 | |
| double Ceph::f0 = 0 |
SV clock parameter (af0)
| double Ceph::f1 = 0 |
SV clock parameter (af1)
| double Ceph::f2 = 0 |
SV clock parameter (af2)
| int Ceph::flag = 0 |
BDS B1C/B2a+B1C/B2b integrity flags.
| int Ceph::iodc = -1 |
BDS CNAV1/CNV2 IODC.
| int Ceph::iode = -1 |
BDS CNAV1/CNV2 IODE.
| 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
| E_SatType Ceph::orb = E_SatType::NONE |
BDS sat/orbit type.
| SatSys Ceph::Sat |
satellite number
| 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
| E_Svh Ceph::svh |
SV health.
| 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
| GTime Ceph::toc = {} |
time of clock
| GTime Ceph::toe = {} |
time of ephemeris, for GPS/QZS, TOE==TOC
| double Ceph::toes = 0 |
TOE (s) in week.
| GTime Ceph::top = {} |
time of prediction
| double Ceph::tops = 0 |
t_op (s) in week
| GTime Ceph::ttm = {} |
transmission time
| double Ceph::ttms = 0 |
transmission time (s) within week
| E_NavMsgType Ceph::type = E_NavMsgType::NONE |
message type
| double Ceph::ura[4] = {} |
user range accuracy GPS/QZS: ura[0]=URAI_NED0, ura[1]=URAI_NED1, ura[2]=URAI_NED2, ura[3]=URAI_ED
| int Ceph::wnop = 0 |
GPS/QZS: GPS week number (of prediction?) with AR.
1.12.0