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Model KG3800 High Accury Single-axis Fiber Optic Gyroscope With 0.5 °/hr Bias Drift

QINGDAO THUNDSEA MARINE TECHNOLOGY CO.,LTD

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Model KG3800 High Accury Single-axis Fiber Optic Gyroscope With 0.5 °/hr Bias Drift

Country/Region china
Categories Level Measuring Instruments
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Product Details

Model KG3800 High Accury Single-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 Shape and installation size

      For every three gyro in gyro mounting holes for 4-4.2 (mm), the other two gyro Ф mounting holes for 4 - the M4 (mm),

      and inlaid steel wire sets

1.4 Weight

      235g±10g

 

1.5 Performance parameters

Index nameIndex requirementsRemarks
Range of measured angular rate(°/s)±800 
Scale Factor Non-linearity at
fixed temperature
(ppm)
≤300 
Asymmetry of Scaling Factor at
Room Temperature
(ppm)
≤300 
Scale Factor Repeatability at
fixed temperature
(ppm)
≤300 
Scale Factor Repeatability at
full temperature range from
-40℃ till 60℃
(ppm)
≤300 
Bias Drift at fixed temperature
(10s,1σ,°/h)
≤0.50 
Bias Drift Repeatability at
fixed temperature
(1σ,°/h)
≤0.50 
Bias Drift Repeatability at
full temperature range from
-40℃ till 60℃
(1σ,°/h)
≤0.50Fixed-point constant
temperature test
Bias Drift at full temperature
range from 40 till 60
(100s,1σ,°/h)
≤0.1Off line compensation
Random Walk
(°/√h)
≤0.125 
Warm up time
(min)
≤2 
Random vibration
(°/h)
≤0.1The difference between the mean
of zero deviation before and after vibration
Shock
(°/h)
≤0.1Zero deviation before and after impact
Resolving power≤0.5 
Zero deviation change before
and after vibration
(°/h)
≤0.3 
Zero bias sensitivity
(°/h/GS)
<0.5 
Storage temperature15℃ ~35℃ 
Operating temperature-40℃ ~70℃ 

 

1.6 Mechanical and electrical interfaces

 

1.6.1 Mechanical interface

        The mounting surface of the product constitutes the fixed surface for external installation, and the mounting screw is M4.

 

1.6.2 Power requirements

Voltage+5V-5V
Precision≤2%≤2%
Ripple(peak)20mV20mV
Maximum current of the gyro for a short time
(<3s)
2A0.2A
Maximum gyro steady-state current
(total temperature)
0.6A0.2A

 

1.6.3 Electrical connection interface

The gyro signal is connected to the system through a lead (0.15mm2, high temperature flame retardant wire, line length 200mm)

 

Physical meaningColour
+5VRed
GNDBlack
-5VWhite
The pulseYelloe
The negative pulseGreen

 

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