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Fiber Optic Gyro

Compact Gyro Fiber Optic Meter , RS422 Output Mode Single Axis Gyro

Name: Compact Gyro Fiber Optic Meter , RS422 Output Mode Single Axis Gyro
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: FCG24
Price: 1600 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	FCG24
MOQ:	1
Price:	1600 USD
Payment Terms:	T/T
Supply Ability:	100/MONTH

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Certification:

Output Mode:

RS422

Range:

≥500°/s

Bias （Allan):

≤0.2°/h

Consumption:

≤0.7w

Power Supply:

5(±0.15)V

Random Walk:

≤0.04°/√h(1σ)

Scale Factor:

4 Mv/° /s

Packaging Details:

Sponge+ box

Supply Ability:

100/MONTH

Highlight:

Compact Fiber Optic Gyroscope

Single Axis Fiber Optic Meter

RS422 Output Single Axis Gyro

Product Description

Compact Gyro Fiber Optic Gyroscope Single Axis Gyro Optic Meter

Table 1 Main Performance Parameters

Items	MFOG24	Unit
Output Signal	RS422
Connector	Welding plate
Axis	1
Consumption	≤1.5	w
Power Supply	5(±0.15)	V
Random walk	≤0.04	°/√h(1σ)
Range	≥500	°/s
Bias (10s,1σ)	≤1.5	°/h
Bias (Allan)	≤0.4	°/h
Bias repeatability(Allan)	≤0.4	°/h
Scale Factor	3600	(LSB/o /s)
Scale factor Non-linearity	≤300	PPM(1σ)
Start up time	≤1	s
Bandwidth	300	Hz
Working Temp.	-45~+70	℃
Store Temp.	-55~+85	℃
Vibration	20~2000,0.04	Hz,g²/Hz
Dimensions	Φ24*40	mm
Weight	≤30	g

FOG-24 micro-nano fiber optic gyroscope (hereinafter referred to as this product) is an angular rate sensor integrating optics with digital output, mechanics and electronics. It is based on the Sagnac effect, integrates a variety of micro-nano fiber devices, and realizes the detection process by detecting, processing and feeding back the phase difference generated by two beams of light propagating in opposite directions.

This product is mainly composed of optical path components, circuit components and structural components. It has the characteristics of simple structure, no moving parts, no wear parts, fast start, small size, light weight and so on. And can be apply to that attitude control and measurement of the carrier.

Composition

A) an optical path assembly;

B) Detection and control signal circuit board;

C) Optical fiber ring skeleton, shell and other structural parts;

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