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MFOG-910 Navigation Grade Fiber Optic Gyroscope 0.8 deg/h Bias Aerospace Inertial Navigation Sensor

Name: MFOG-910 Navigation Grade Fiber Optic Gyroscope 0.8 deg/h Bias Aerospace Inertial Navigation Sensor
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: MFOG-910
Price: 10000 USD
Availability: InStock

Brand Name:	FIREPOWER
Model Number:	MFOG-910

Detail Information

Product Description

Detail Information

Place of Origin:

China

Certification:

ISO 9001:2015, CE, RoHS

Zero-bias Stability:

0.8 Deg/h

Bias Repeatability:

0.8 Deg/h

Measurement Range:

240 Deg/s

Scale Factor Nonlinearity:

<=1000 Ppm

Size:

82mm X 82mm X 19.5mm

Acceleration:

>=70g

Highlight:

navigation grade fiber optic gyroscope

aerospace inertial navigation FOG sensor

0.8 deg/h bias MFOG-910 gyro

Product Description

MFOG-910 Navigation Grade Fiber Optic Gyroscope for Aerospace Inertial Navigation

The MFOG-910 is a navigation-grade fiber optic gyroscope integrating optical, mechanical, and electronic technologies in a compact 82mmx82mmx19.5mm package. Utilizing the Sagnac effect with micro-nano fiber-optic devices, it delivers precise 0.8 deg/h bias stability for demanding aerospace inertial navigation systems.

Engineered with no moving or wearing components, the MFOG-910 ensures rapid startup, exceptional reliability, and consistent performance across wide temperature ranges. Its 1000Hz bandwidth and 0.02 deg/rt-h random walk make it the preferred choice for flight control computers and navigation-grade IMU integration.

Technical Specifications

Parameter	Specification
Range (deg/s)	+/-240
Scale Factor (mV/deg/s)	47+/-5
Scale Factor Nonlinearity (ppm)	<=1000
Zero-Bias Stability (10s, 1 sigma, deg/H)	<=0.8
Zero-Bias Repeatability (1 sigma, deg/H)	<=0.8
3dB Bandwidth (Hz)	>=1000
Random Walk (deg/rt-H)	<=0.02
Power Supply (V)	5+/-0.25+12
Power Consumption (W)	<=1.5
Impact Resistance (g)	>=1500
Vibration Resistance (g)	>=70
Service Life (years)	>=15
MTBF (Calculated)	>=100,000 hours

Key Features

Navigation-grade 0.8 deg/h bias stability for precision INS
High 1000Hz bandwidth for dynamic flight maneuver sensing
Ultra-low 0.02 deg/rt-h angular random walk
Solid-state micro-nano design with no moving parts
1500g impact and 70g vibration resistance
100,000+ hour MTBF with 15-year service life

Applications

Aerospace inertial navigation systems, flight control computers, navigation-grade IMU integration, launch vehicle guidance, spacecraft attitude determination, high-altitude UAV autopilot.

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

Gyro North Finder

Magnetometer Sensor

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

Gyro North Finder

Magnetometer Sensor

products details

MFOG-910 Navigation Grade Fiber Optic Gyroscope 0.8 deg/h Bias Aerospace Inertial Navigation Sensor

MFOG-910 Navigation Grade Fiber Optic Gyroscope 0.8 deg/h Bias Aerospace Inertial Navigation Sensor

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