Low Cost FOG Gyroscope

ER-FOG-910 (0.02º/h)
1. Bias stability: 0.02º/h;
2. Small size: Φ82×26;
3. Long life and high reliability.

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Introduction

ER-FOG-910 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

Specifications

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.