Space Vehicle Configuration
Satellite Navigation
76
User Manual 1178.6379.02 ─ 01
Parameter
Remote command:
Cosine Difference of Latitude - C
uc
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:CUC
Sine Difference of Latitude - C
us
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:CUS
Cosine Difference of Orbital Radius - C
rc
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:CRC
Sine Difference of Orbital Radius - C
rs
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:CRS
Cosine Difference of Inclination - C
ic
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:CIC
Sine Difference of Inclination - C
is
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:CIS
QZSS SV
Comprises the navigation message parameters, specific to and common for all QZSS
satellites.
Simulated Orbit ← QZSS SV
Comprises the navigation message parameters, specific to and common for all QZSS
satellites.
Parameter
Remote command:
Reference Week
[:SOURce<hw>]:BB:GNSS:SVID<ch>:QZSS:
SIMulated:ORBit:WNOE
Reference Time of Week
[:SOURce<hw>]:BB:GNSS:SVID<ch>:QZSS:
SIMulated:ORBit:TOE
Square Root of Semi-Major Axis - A
1/2
[:SOURce<hw>]:BB:GNSS:SVID<ch>:QZSS:
SIMulated:ORBit:SQRA
Eccentricity - e
[:SOURce<hw>]:BB:GNSS:SVID<ch>:QZSS:
SIMulated:ORBit:ECCentricity
Inclination Angle - i
0
[:SOURce<hw>]:BB:GNSS:SVID<ch>:QZSS:
SIMulated:ORBit:IZERo
Longitude of Ascending Node - Ω
0
[:SOURce<hw>]:BB:GNSS:SVID<ch>:QZSS:
SIMulated:ORBit:OZERo
Argument of Perigee -
ω
[:SOURce<hw>]:BB:GNSS:SVID<ch>:QZSS:
SIMulated:ORBit:OMEGa
Mean Anomaly - M
0
[:SOURce<hw>]:BB:GNSS:SVID<ch>:QZSS:
SIMulated:ORBit:MZERo
Rate of Inclination Angle - i'
[:SOURce<hw>]:BB:GNSS:SVID<ch>:QZSS:
SIMulated:ORBit:IDOT
Simulated Orbit and Orbit Perturbation Settings