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Principals of Operation
7 - 3
GENERATOR (cont)
NAV Data:
Navigation Data is computed in real-time to match the simulation
Positional Simulation:
Maximum Relative Velocity (Range Rate) ± 1000 kts
Maximum Relative Jerk ± 500 m/s3
Maximum Altitude 100,000 ft
Positional Simulation
Accuracy:
Pseudorange <2mm (RMS)
Pseudorange Rate <1mm/s (RMS) with respect to master oscillator
Pseudorange Jerk ±0.02 m/s3 (RMS over >1s)
Delta Pseudorange <2mm (RMS)
Interchannel Code Phase Alignment ± 0.02 m (RSS)
Interchannel Carrier Phase Alignment ± 0.265mm (RSS)
7.2
MASTER OSCILLATOR
Frequency:
10 MHz nominal (* see note)
Temperature Stability:
± ±0.05 ppm
Aging Rate:
±0.3 ppm/yr, ± 2.5 ppm/ 10 yr
Uncertainty:
±1 ppm
External Reference Input
Input Level:
0.25 to 6.0 Vp-p
Input Impedance
:50 ohm nominal
Input Frequency:
10.0 MHz ±10 Hz
External Reference Output
Output Level:
1.5 Vp-p nominal into 50
Output Frequency:
10.0 MHz nominal
Reliability
MTBF:
>10000 hrs
MTTR:
1hr
7.3
COUPLER
Type:
Patch in RF Absorbent Foam
Coupling:
-21.5 dB typical at 1575.420 MHz.
Isolation:
>
25 dB at 1575.42 MHz
> 30 dB typical at 1575.42 MHz
Содержание 87339
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Страница 127: ...Principals of Operation 6 10 Fig 6 12 GPS Code Correlation Process Fig 6 13 GPS Nav Data Recover by Moduo 2 Addition...
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Страница 187: ...E 6 The Simulation will run until the end of the Trajectory File Figure E 10 Fig E 10 Trajectory Simulation Complete...
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