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Product Details:
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| Range Of Measured Angular Rate (deg/s): | ±400 | Scale Factor Non-linearity At Fixed Temperature (ppm): | ≤50 |
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| Scale Factor Asymmetry At Room Temperature (ppm): | ≤50 | Scale Factor Repeatability At Fixed Temperature (ppm): | ≤50 |
| Scale Factor Repeatability At Full Temperature Range Form －40℃till 60℃ (ppm): | ≤200 | Bias Drift At Fixed Temperature (10s,1σ,°/h): | ≤0.05 |
| Bias Drift Repeatability At Fixed Temperature (1σ,°/h): | ≤0.03 | Bias Drift Repeatability At Full Temperature Range Form －40℃till 60℃ (1σ,°/h): | ≤0.05 |
| Bias Drift At Full Temperature Range From －40℃till 60℃ (100s,1σ,°/h): | ≤0.1 | Random Walk Coefficient (°/√h): | ≤0.008 |
| Standby Time (min): | 0 | Random Vibration (°/h): | ≤0.1 |
| Shock (°/h): | ≤0.1 | ||
| High Light: | 20mV Single axis inertial gyroscope,0.05 °/hr marine gyroscope,20mV mems based gyroscope |
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Model F70HA High Accury Single-axis Fiber Optic Gyroscope With 0.05 °/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 Dimensions
Outline size (70 ± 0.1)mm × (70 ± 0.1) mm × (31. 8 ± 0.1)mm,
Installation dimension (58 ± 0.05 mm) × (58 ± 0.05mm)
1.4 Weight
300 g±20g
1.5 Performance parameter
| Index name | Index requirements | Remarks |
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Range of measured angular rate (deg/s) |
±400 | |
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Scale Factor Non-linearity at fixed temperature (ppm) |
≤50 | |
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Scale factor asymmetry at room temperature (ppm) |
≤50 | |
|
Scale Factor Repeatability at fixed temperature (ppm) |
≤50 | |
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Scale Factor Repeatability at full temperature range form －40℃till 60℃ (ppm) |
≤200 | |
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Bias Drift at fixed temperature (10s,1σ,°/h) |
≤0.05 | |
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Bias Drift Repeatability at fixed temperature (1σ,°/h) |
≤0.03 | |
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Bias Drift Repeatability at full temperature range form －40℃till 60℃ (1σ,°/h) |
≤0.05 |
Fixed-point constant temperature test |
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Bias Drift at full temperature range from －40℃till 60℃ (100s,1σ,°/h) |
≤0.1 | Off line compensation |
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Random Walk Coefficient (°/√h) |
≤0.008 | |
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Standby time (min) |
0 | |
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Random Vibration (°/h) |
≤0.1 |
The difference between the mean of zero deviation before and after vibration |
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Shock (°/h) |
≤0.1 | Zero deviation before and after impact |
1.6 Mechanical and Electrical Interfaces
1.6.1 Mechanical Interface
The product installation surface is a fixed surface for external installation, and the installation screw is M6.
1.6.2 Power Supply Requirements
DC power supply: ± (5 V ± 0.25V)
Ripple: 20mV
Output power: ≥5W
Contact Person: Yu.Jing
Tel: +8613045000776
