Space Vehicle Configuration
Satellite Navigation
75
User Manual 1178.6379.02 ─ 01
Parameter
Remote command:
Y''
n
[:SOURce<hw>]:BB:GNSS:SVID<ch>:GLONass:SIMulated:ORBit:YDDN
Z''
n
[:SOURce<hw>]:BB:GNSS:SVID<ch>:GLONass:SIMulated:ORBit:ZDDN
BeiDou SV
Comprises the navigation message parameters, specific to and common for all BeiDou
satellites.
Simulated Orbit ← BeiDou SV
Comprises the navigation message parameters, specific to and common for all BeiDou
satellites.
Parameter
Remote command:
Reference Week
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:WNOE
Reference Time of Week
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:TOE
Square Root of Semi-Major Axis - A
1/2
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:SQRA
Eccentricity - e
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:ECCentricity
Inclination Angle - i
0
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:IZERo
Longitude of Ascending Node - Ω
0
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:OZERo
Argument of Perigee -
ω
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:OMEGa
Mean Anomaly - M
0
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:MZERo
Rate of Inclination Angle - i'
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:IDOT
Rate of Right Ascension - Ω'
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:ODOT
Mean Motion Difference - Δ
n
[:SOURce<hw>]:BB:GNSS:SVID<ch>:BEIDou:
SIMulated:ORBit:NDELta
Orbit Perturbation ← BeiDou SV
Comprises the navigation message parameters, specific to and common for all BeiDou
satellites.
Simulated Orbit and Orbit Perturbation Settings