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High Stability Single Axis Fiber Optic Gyro with RS422 Output for Navigation System

Name: High Stability Single Axis Fiber Optic Gyro with RS422 Output for Navigation System
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: MFOG-1703
Price: 10000.00 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	MFOG-1703
MOQ:	1
Price:	negotiable
Payment Terms:	T/T
Supply Ability:	200/MONTH

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Certification:

Dynamic Range:

±150°/s

Zero Bias Stability:

≤1°/h

Zero-bias Repeatabilitytime:

≤1°/h

Random Walk Coefficient:

≤0.02°/ √h

Scale Factor Nonlinearity:

≤30ppm

Vibration:

20~2000Hz,0.06g²/Hz

Interface:

RS-422

Power Supply:

5+0.25V

Packaging Details:

Sponge+ box

Supply Ability:

200/MONTH

Highlight:

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Product Description

High Stability Single Axis Fiber Optic Gyro with RS422 Output for Navigation System

The MFOG-1703 fiber optic gyroscope utilizes the Sagnac effect for precise angular rate detection, offering high sensitivity and thermal stability. Its compact design and fast startup make it suitable for aerospace research, UAV attitude reference systems, and precision instrumentation. Compatible with Fizoptika VG1703 in both interface and performance.

Composition

Optical path assembly
Detection and control signal circuit board
Optical fiber ring skeleton, shell and other structural parts

Appearance and Dimensions

Shape: Cylindrical

Dimensions: φ40mm × 20mm

Mounting: 3 M3 threads on the bottom for external connection

Physical Specifications

Weight: ≤40g

Operating Temperature: -40℃ to +70℃

Storage Temperature: -55℃ to +85℃

Random Vibration: 20g, frequency range: 20Hz to 2000Hz

Main Performance Parameters

Serial Number	Project	Performance Indicators
1	Range (°/s)	±150
2	Scale factor (mV/°/s)	12±1.2
3	Zero-bias stability (10s, 1σ, °/h)	≤1
4	Zero-bias repeatability (1σ, °/h)	≤1
5	Angular random walk (°/h 1/2)	≤0.02
6	Zero-bias temperature sensitivity (uV/°C)	≤1
7	Scale Factor Temperature Sensitivity (ppm/°C)	≤300
8	3dB Bandwidth (Hz)	≥450
9	Impact (g)	1200, 1ms, half sine
10	Power supply (V)	5+0.25
11	Power Consumption (W)	≤1
12	Dimension (mm)	φ40 × 20

Tags:

Accelerometer Gyro Sensor

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Fiber Optic Gyro

Inertial Navigation System

Gyro North Finder

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High Stability Single Axis Fiber Optic Gyro with RS422 Output for Navigation System

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