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3 In 1 Fiber Optic Gyro FOG Inertial Gyroscope Navigation

Shenzhen Avionics Technology Co.,Ltd

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Address: 803, Block A, Building B5-1, Junfeng Industrial Complex, HepingCommunity, Fuhai Street, Bao an District, Shenzhen

Contact name:Caine

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3 In 1 Fiber Optic Gyro FOG Inertial Gyroscope Navigation

Country/Region china
City & Province shenzhen
Categories Projectors
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Product Details

triaxial gyro inertial navigation gyro 3 in 1 FOG integrated gyro

 

 

Performance Characteristics

No.Test itemUnitTechnical requirements
1Start timeminPower-on bias stability index
2Zero bias stability(°)/h≤ 0.05 (10s smoothing)≤ 0.015 (100s smoothing)
3Zero bias stability at full temperature(1 ℃/min variable temperature, 100 s average)(°)/h≤0.08
4Zero-bias repeatability(°)/h≤0.015
5Random walk coefficient(º)/h1/2≤0.003
6Scale factor nonlinearityppm≤20
7Scale factor asymmetryppm≤5
8Scale factor repeatabilityppm≤10
9Scale factor repeatability (full temperature)ppm≤50
10Operating temperature-40~+60
11Storage temperature-50~+70
12Dynamic range(°)/s±500
13Supply voltageV+5V
14Steady state power consumption (full temperature)W<4

 

 

This product is an inertial angular rate sensor based on the optical Sagnac effect, which is used to measure the angular velocity of the carrier along the sensitive axis of the product. The angular velocity sensing unit of the product is an optical fiber ring, and a digital closed-loop detection circuit is adopted to extract the optical path difference of clockwise and counterclockwise propagation light caused by the external physical angular velocity, which is sensed by the optical fiber ring,At the same time, the voltage signal converted from the optical path difference signal is used for closed-loop feedback and control to realize the modulation and demodulation of the signal and achieve the purpose of high-precision angular velocity signal detection.

 

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