Low Cost FOG Gyroscope

Author:ericcointernational 2024-03-06 15:19:07 61 0 0

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

Specificaions

ParametersUnitTypical valueMaximum
Measurement range(º)/s±1000/
Bias(º)/h/5
Run-up time1s35
Bias stability(stable temperature)(º)/h0.020.05
Bias stability(stable temperature)(º)/h0.30.5
Bias repeatability(º)/h0.30.5
Temperature sensitivity@1℃/min(º)/h0.010.03
Random walk coefficient(stable temperature)(º)/h 1/20.010.03
Scale factorLSB/(º/s)2×10420000±1000
Scale factor non-linearityppm2050
Scale factorppm2050
Bandwidthdb-3≥1000
DimensionmmΦ82×26/
Weightg<250/
Output voltageV+5~+40/
Power consumptionW1.6 (typical) 4 (max)/
Operating temperature-40~+60/
Storage temperature-50~+70/
Vibration/6.06g, 20Hz~2000Hz/
Mean time between failuresh20000/
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.


Comments   Please sign in or sign up to post.

0

0 of 500 characters used

Copyright:@2020-2021