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FG40T Navigation Grade Fiber Optic Gyroscope

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Introduction

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I Introduction

The Inertial Measurement Unit (IMU) features advantages such as compact size, light weight, low power consumption, and high precision. It can be used to design pure strapdown, single-axis, and dual-axis modulated inertial navigation systems, meeting the demand for small-size, high-precision inertial navigation equipment in new unmanned platforms, underwater/torpedo weaponry, as well as land-based and airborne weapon platforms. It possesses the capability for dynamic measurement of carrier angular and linear motion information.

II.Technical Parameters

Item

Indicator

Description

Parameter

Remark

Gyro

Zero Bias

Bias Stability (10s)

0.1°/h

 

Zero Bias Stability at Variable Temperature (100s)

0.5°/h

 

Scaling Factor

Scale Factor Nonlinearity

≤20ppm

 

Other Indicators

Random Walk Coefficient

0.01°/½h

 

Input Range

400°/s

 

Features

Environmental Performance

Operating Temperature

-40℃60℃

 

Storage Temperature

-45℃70℃

 

General Requirements

Power Supply

5VDC

 

Stable Power Consumption

≤4W

Startup Power Consumption ≤10W

Dimensions(mm)

64.5×65.2×46.5

 

Weight

≤330g

 

III Electrical Interface Definition  (J30JZLN9ZKCA000)

Pinout

Signal

Type

Description

Remark

1,6

+5V

Input

Power Input

+5V

2,7

GND

Input

 

5

RS422_TX1+

Output

RS422 Serial Port 1

 

9

RS422_TX1-

Output

IMU Raw Data

4

RS422_RX1+

Input

 

8

RS422_RX1-

Input

 

IV Structure Diagram

 


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