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Inertial Angular Rate Sensor Integrated Optic Gyroscope Sagnac Effect

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Shenzhen Fire Power Control Technology Co., LTD

City: shenzhen

Province/State:guangdong

Country/Region:china

Tel:86-755-23097872

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Inertial Angular Rate Sensor Integrated Optic Gyroscope Sagnac Effect

Brand Name Firepower
Model Number F50A
Place of Origin CHINA
Minimum Order Quantity 1
Price Negotiable
Payment Terms T/T
Supply Ability 200/MONTH
Delivery Time 30 DAYS
Packaging Details Sponge+ box
Measuring Range -500°/s~+500°/s
Zero-bias repeatability <=0.1°/h
Zero-bias stability <=0.1°/h
Bandwidth >200Hz
Initialization time <5S
Communication Mode RS422
Operating temperature -45℃~+60℃
Storage temperature -55℃~+75℃
Scale factor nonlinearity <50ppm
Scale factor repeatability <50ppm
Supply voltage 5v
Detailed Product Description

Inertial Angular Rate Sensor Optical Sagnac Effect Fiber Gyro

 

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. The 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 the external physical angular rate, which is 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 angular rate signal detection is achieved.

 

This product is composed of an optical angular velocity sensing unit and a signal detection unit, providing single-axis angular increment information and internal temperature information.

 

The products are mainly suitable for applications such as medium-precision inertial navigation systems, positioning and orientation systems, and servo stabilization systems.

 

 

The main components of the product are as follows:

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

Overall dimension (mm): 50 ± 0.1 × 50 ± 0.1 × 32 ± 0.1 (L × W × H);

Installation dimension (mm): 43 ± 0.1 × 43 ± 0.1 (L × W), Φ3.2mm × 4, such asFigure As shown.

 

Main Parameters

Serial numberTest itemUnitTechnical requirements
1Overall dimensionsmm50×50×32
2Start time55s
3

Zero bias stability

(10s smooth)

(°)/h≤0.1
4Zero-bias repeatability(°)/h≤0.1
5Random walk coefficient(º)/h1/2≤0.01
6Scale factor nonlinearityppm≤50
7Scale factor repeatabilityppm≤50
8Operating temperature-40~+70
9Storage temperature-50~+70
10Dynamic range(°)/s±500
11Supply voltageV+5V
12Steady state power consumption (full temperature)W<4
13BandwidthHz≥200

 

F50A FOB MANUAL.pdf

 
Product Tags: UAV integrated optic gyroscope   sagnac effect integrated optic gyroscope  
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