Low Cost FOG Gyroscope
Product Description
ER-FOG-910 Low Cost FOG Gyroscope
Low Cost FOG Gyroscope Features
Low consumption, normal temperature consumption 1.6W
Quickly star-up, small offset drift
Signal power supply, wide voltage (5.5V~40V), simplified system design
Support full digital RS-422/RS-232 electronic interface output
Long life and high reliability, mean time between failures exceeds 20000h
Applications
Drone flight control
Inertial measurement unit
Surveying and mapping, track inertial traverse road test
Photoelectric pod
Platform stabilizer
FOG Gyroscope Specificaions
Parameters | Unit | Typical value | Maximum |
Measurement range | (º)/s | ±1000 | / |
Bias | (º)/h | / | 5 |
Run-up time1 | s | 3 | 5 |
Bias stability2 (stable temperature) | (º)/h | 0.02 | 0.05 |
Bias stability3 (stable temperature) | (º)/h | 0.3 | 0.5 |
Bias repeatability | (º)/h | 0.3 | 0.5 |
Temperature sensitivity@1℃/min | (º)/h | 0.01 | 0.03 |
Random walk coefficient2 (stable temperature) | (º)/h 1/2 | 0.01 | 0.03 |
Scale factor | LSB/(º/s) | 2×104 | 20000±1000 |
Scale factor non-linearity | ppm | 20 | 50 |
Scale factor | ppm | 20 | 50 |
Bandwidth | db | -3 | ≥1000 |
Dimension | mm | Φ82×26 | / |
Weight | g | <250 | / |
Output voltage | V | +5~+40 | / |
Power consumption | W | 1.6 (typical) 4 (max) | / |
Operating temperature | ℃ | -40~+60 | / |
Storage temperature | ℃ | -50~+70 | / |
Vibration | / | 6.06g, 20Hz~2000Hz | / |
Mean time between failures | h | 20000 | / |
External connector | / | 10P rectangular connector | / |
External electrical interface | / | RS-422、RS-232 | / |
Note1: Refers to the time from booting to reaching the performance index.
Note2: The bias stability and the random walk coefficients are measured by the allan variance analysis under the laboratory steady temperature conditions.
Note3: The GJB-2426A method is used for statistics, and the relevant time is 10s.
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