Perturbations and Errors Simulation
Satellite Navigation
122
User Manual 1178.6379.02 ─ 01
Parameter
Remote command:
AODE
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:NMESsage:DNAV:
EPHemeris:IODE
Reference Time of Ephem-
eris - t
0e
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:NMESsage:DNAV:
EPHemeris:TOE
Square Root of Semi-Major
Axis - A
1/2
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:NMESsage:DNAV:
EPHemeris:SQRA
Eccentricity - e
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:NMESsage:DNAV:
EPHemeris:ECCentricity
Inclination Angle - i
0
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:NMESsage:DNAV:
EPHemeris:IZERo
Longitude of Ascending
Node - Ω
0
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:NMESsage:DNAV:
EPHemeris:OZERo
Argument of Perigee -
ω
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:NMESsage:DNAV:
EPHemeris:OMEGa
Mean Anomaly - M
0
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:NMESsage:DNAV:
EPHemeris:MZERo
Rate of Inclination Angle - i'
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:NMESsage:DNAV:
EPHemeris:IDOT
Rate of Right Ascension -
Ω'
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:NMESsage:DNAV:
EPHemeris:ODOT
Mean Motion Difference -
Δ
n
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:NMESsage:DNAV:
EPHemeris:NDELta
BeiDou > Orbit Perturbation
Comprises the parameters of the BeiDou satellites.
Parameter
Remote command:
Cosine Difference of Latitude - C
uc
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
NMESsage:DNAV:EPHemeris:CUC
Sine Difference of Latitude - C
us
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
NMESsage:DNAV:EPHemeris:CUS
Cosine Difference of Orbital Radius - C
rc
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
NMESsage:DNAV:EPHemeris:CRC
Sine Difference of Orbital Radius - C
rs
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
NMESsage:DNAV:EPHemeris:CRS
Cosine Difference of Inclination - C
ic
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
NMESsage:DNAV:EPHemeris:CIC
Sine Difference of Inclination - C
is
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
NMESsage:DNAV:EPHemeris:CIS
Orbit
Comprises the parameters of the QZSS satellites.
Orbit and Orbit Perturbation Errors Settings