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Three Axis Fiber Optic Gyroscope

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Three Axis Fiber Optic Gyroscope

Three Axis Fiber Optic Gyroscope
Three Axis Fiber Optic Gyroscope

Large Image :  Three Axis Fiber Optic Gyroscope

Product Details:
Place of Origin: China
Brand Name: THUNDSEA
Certification: CCS
Model Number: F3X50B

Three Axis Fiber Optic Gyroscope

Drawtube: Binocular
High Light:

Three Axis optical gyroscope


mechanical electronic gyroscope


solid state digital gyroscope

Model F3X50B High Accury There-axis Fiber Optic Gyroscope With 0.5 °/hr Bias Drift


1. Product Introduction


1.1 Working Principle and Function

This product is an inertial angular rate sensor based on the principle of Sagnac effect, which is used to measure the angular rate movement of the carrier around the sensitive axis of this sensor. This unit takes the fiber optic coil as the angular rate sensitive unit and the closed-loop detection circuit as the basis.

Two beams from a laser are injected into the same fibre but in opposite directions. Due to the Sagnac effect, the beam travelling against the rotation experiences a slightly shorter path delay than the other beam. The resulting differential phase shift is measured through interferometry, thus translating one component of the angular velocity into a shift of the interference pattern which is measured photometrically.

Beam splitting optics launches light from a laser diode into two waves propagating in the clockwise and anticlockwise directions through a coil consisting of many turns of optical fibre. The strength of the Sagnac effect is dependent on the effective area of the closed optical path: this is not simply the geometric area of the loop but is enhanced by the number of turns in the coil.

This product is an inertial sensor composed of optical system, corresponding power supply and data processing circuit. It can provide three-axis angle increment information.


1.2 Configuration

The product is mainly composed of the following components:

a) Optical part: light source, coupler, Y modulator, fiber coil, detector;

b) Circuit part: processor board, light source board and preamplifier;

c) Structural part: body, cover, etc.


1.3 Size

Outward dimension: Φ(79.5 ± 0.1) mm × (79.5 ± 0.1) mm × (49.8 ± 0.1) mm,

Mounting size: (73.0 ± 0.1) mm ×( 73.0 ± 0.1) mm,


Three Axis Fiber Optic Gyroscope 0

1.4 Weight

     500g ± 30g


1.5 Performance

Item   Remarks
Scale factor Non-linearity at
fixed temperature
Scale factor repeatability at
fixed temp
Start-up time(s) ≤2  
Standby time(s) ≤30  
Bias drift at fixed temp
Bias drift repeatability
Bias drift at full temp
Random walk(°/√h) ≤0.1  
Misalignment angle of input
≤20 Full temperature range
Threshold(°/h) ≤0.5  
Resolution ≤0.5  
Bias magnetic sensitivity
Bandwidth(HZ) ≥200 Design assurance
Output delay time(μs) ≤1000  
Average values of bias before,
duing and after vibration
Bias after vibration difference
from vibration before(°/h)


1.6 Mechanical and electrical interfaces


1.6.1 Mechanical interface

Four M3 Screws of the mounting side.


1.6.2 Power Supply and Power Consumption

Voltage Voltage range Ripple(RMS) Current
+5V ±5% ≤50mV >3.00A(start-up)


Power consumption: working status <5W at room temperature, <8W at full temp

Start-up status: ≤ 10W


1.6.3 Electrical Connection Interface

FIG 3 Definition of connector (Model J30J-25ZKP3)

Serial number Signal Contact number Remarks
1 +5V 1,2 Gyroscope power supply
2 GND 3,15
3 TX+ 10,22 RS422TX
4 TX- 11,23
5 TR+ 12,24 RS422 RX
6 TR- 13,25


Three Axis Fiber Optic Gyroscope 1Three Axis Fiber Optic Gyroscope 2Three Axis Fiber Optic Gyroscope 3

Contact Details

Contact Person: Yu.Jing

Tel: +8613045000776

Fax: 86-532-68977475

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