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Navigation Grade Fiber Optic Gyroscope FOG)Sensor for Aerospace Inertial Navigation System

Categories Accelerometer Gyro Sensor
Brand Name: FIREPOWER
Model Number: MFOG-910
Place of Origin: China
MOQ: 1
Price: 500$
Payment Terms: L/C,T/T
Supply Ability: 500/month
Delivery Time: 1 week for sample
Packaging Details: sponge +carton
Measurement Range: 240°/s
Bias Repeatability: 0.8°/h
Size: 82mmx82mmx 19.5mm
Zero-bias stability: 0.8°/h
Scale factor nonlinearity: ≤1000ppm
Acceleration: ≥70g
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Navigation Grade Fiber Optic Gyroscope FOG)Sensor for Aerospace Inertial Navigation System

MFOG-910 Micro-Nano Fiber Optic Gyroscope

The MFOG-910 Micro-Nano Fiber Optic Gyroscope (hereinafter referred to as "the product") is an angular rate sensor that integrates optics, mechanics, and electronics. Based on the Sagnac effect, it incorporates various micro-nano fiber-optic devices to detect, process, and feedback the phase difference generated by two counter-propagating beams of light, thereby achieving precise angular rate measurement.

The product is primarily composed of optical path assemblies, electronic circuits, and mechanical structures. It features a simple design with no moving or wearing parts, ensuring fast startup, compact size, lightweight construction, and high reliability. It is suitable for attitude control and motion measurement in various carrier systems


Main Performance Parameters

Serial number

Project

Performance indicators

1

Range (°/s)

±240

2

Scale factor (mV/ o /s)

47±5

3

Scale factor nonlinearity (ppm)

≤1000

4

Zero-bias stability (10s, 1σ, o /H)

≤0.8

5

Zero-bias repeatability (1σ, o /H)

≤0.8

6

3dB Bandwidth (Hz)

≥1000

7

Random walk ( o /√ H)

≤0.02

8

Power supply (V)

5+0.25

+12

9

Power Consumption (W)

≤1.5

10

Impact (g)

≥1500

11

(g)

≥70

12

Life (years) (calculated assessment)

≥15

13

MTBF (Calculated Assessment)

≥100000


Installation Dimensions

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