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High Precision 3 Axis Inertial Fiber Optic Gyro Sensor With Optical Modulator

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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High Precision 3 Axis Inertial Fiber Optic Gyro Sensor With Optical Modulator

Country/Region china
City & Province shenzhen
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Product Details

High-Precision 3-Axis Inertial Fiber Optic Gyro Sensor with Optical Modulator

 

Dimensions

 

Overall dimension of circuit box (mm): (96 ± 0.1) × (96 ± 0.1) × (32.9 ± 0.1) (L × W × H);

Dimension of optical fiber sensing unit (mm): Ф92 × 27;

Installation dimension of circuit box (mm): (88 ± 0.1) × (84 ± 0.1) (L × W), Φ4mm × 4;

Installation dimension of optical fiber sensing unit:

Such asFig. 2 Schematic diagram of installation of sensing unitAs shown.

Performance Characteristics

 

Serial numberTest itemUnitTechnical requirements
1Measuring rangeº/s±300
2

Zero bias stability at room temperature

(100s smoothing, 1σ)

º/h≤0.01
3Zero-bias repeatabilityº/h≤0.01
4Random walk coefficientº/h1/2≤0.001
5Scale factor repeatabilityppm≤100
6Operating temperature-40~+60
7Storage temperature-50~+70
8Supply voltageV+5V
9BandwidthHz>200
10Steady-state power consumptionW≤7
11Start timemin1
12Startup instantaneous power consumptionW

≤ 10 (within 3s after power on)

 

 

 

 

This product is an inertial angular rate sensor based on the optical Sagnac effect, which is used to measure the angular rate of the carrier along the sensitive axis of the product. An angular rate sensing unit of the product is an optical fiber ring, a digital closed loop detection circuit is adopted to extract the optical path difference of clockwise and counterclockwise propagation light caused by external physical angular rate and sensed by the optical fiber ring, and meanwhile, a voltage signal converted from an optical path difference signal is subjected to closed loop feedback and control, so that the modulation and demodulation of the signal are realized, and the purpose of high-precision angular rate signal detection is achieved.

 

This product consists of an optical angular velocity sensing unit and a signal detection unit, and provides information of three-axis angular increment and internal temperature.

The products are mainly suitable for high-precision inertial navigation systems, positioning and orientation systems and other applications.

 

The main components of the product are as follows:

  1. The optical path unit comprise an erbium fiber light source, an optical fib ring, an integrated optical phase modulator, an optical fiber coupler and a photodetector;
  2. The circuit unit comprises a light source driving circuit and a detection and control signal circuit board;
  3. Gyroscope structural parts.

Pin definition

Point number

Definition

Comment

1,9+5VPower supply input
2,10GNDPower ground
8SEL+Gyroscope gating power supply, connected to high level + 5V
15SEL-Gyro gating signal
6TXD+Gyro differential output positive
14TXD+Gyro differential output negative
3,4,5,7,11,12,13——Reserved

Gyro gating power is externally connected with + 5V, and the gating signal is TTL level.

 

 

 

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