Single-Axis Angular Rate Gyro Sensor for Inertial Navigation System

Product Details
Customization: Available
Type: Servo
Output Signal Type: Digital Output
Manufacturer/Factory, Trading Company
Gold Member Since 2023

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Registered Capital
1000000 RMB
Plant Area
1001~2000 square meters
  • Single-Axis Angular Rate Gyro Sensor for Inertial Navigation System
  • Single-Axis Angular Rate Gyro Sensor for Inertial Navigation System
  • Single-Axis Angular Rate Gyro Sensor for Inertial Navigation System
  • Single-Axis Angular Rate Gyro Sensor for Inertial Navigation System
  • Single-Axis Angular Rate Gyro Sensor for Inertial Navigation System
  • Single-Axis Angular Rate Gyro Sensor for Inertial Navigation System
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Basic Info.

Model NO.
F-60
Measuring Shaft Quantities
Single
Accuracy Grade
0.1deg/H
IP Rating
IP67
Certification
CE
Customized
Customized
Measuring Range
1000deg/S
Bias Stability 10s,1σ, °/H
<0.1deg/H
Bias Repeatability
<0.1deg/H
Start Time
5s
Random Walk
<0.01deg/H1/2
Power Supply
5V
Working Temp
-40~70
Transport Package
Sponge and Box
Specification
60 X 60 X 31mm
HS Code
9031809090
Production Capacity
500/Month

Product Description

Single-axis Angular Rate Gyro Sensor for Inertial Navigation System

Specifications
No. Test item Unit Technical requirements
1 Overall dimensions mm 60×60×31
2 Start time s 5
3 Zero bias stability
(10 s smoothing, 1σ)
º/h ≤0.1
4 Zero-bias repeatability º/h ≤0.1
5 Random walk coefficient º/h1/2 ≤0.01
6 Scale factor nonlinearity ppm ≤50
7 Scale factor repeatability ppm ≤50
8 Operating temperature ºC -40~+70
9 Storage temperature ºC -50~+70
10 Dynamic range (°)/s ±1000
11 Supply voltage V +5
12 Steady-state power consumption W <4
 
  1. Overview
This document specifies the requirements and methods for the use and maintenance of FOG-60 fiber optic gyroscope (product for short).
  1. Product introduction
    1. Working principle, function and scope of application of the product
      1. How it works
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, and a digital closed-loop detection circuit is adopted to extract the optical path difference of clockwise and anticlockwise propagating light caused by the external physical angular rate, 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 angular velocity signal detection.
      1. Function
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.
      1. Scope of application
The products are mainly suitable for applications such as medium-precision inertial navigation systems, positioning and orientation systems, and servo stabilization systems.
    1. Composition
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.
    1. Appearance and installation dimension
Overall dimension (mm): (60 ± 0.1) × (60 ± 0.1) × (31 ± 0.1) (L × W × H);
Installation dimension (mm): (50 ± 0.1) × (50 ± 0.1) (L × W), Φ3.2mm × 4, such asFigure 1As shown.



Size
Single-Axis Angular Rate Gyro Sensor for Inertial Navigation SystemSingle-Axis Angular Rate Gyro Sensor for Inertial Navigation System

Comany and production
Single-Axis Angular Rate Gyro Sensor for Inertial Navigation System
Single-Axis Angular Rate Gyro Sensor for Inertial Navigation System


















  





 
 
 

 

 

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