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F41IMU Fiber Optic Inertial Unit

Keyword:

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)

0.3°/h

 

Zero Bias Stability at Variable Temperature (100s)

0.5°/h

 

Scaling Factor

Scale Factor Nonlinearity

≤20ppm

 

Other Indicators

Random Walk Coefficient

0.02°/½h

 

Input Range

400°/s

 

Accelerometer

Deviation

Zero Bias Repeatability

0.3mg

 

Zero Bias

Bias Temperature Sensitivity

50μg/℃

 

Scaling Factor

Scale Factor Repeatability

300ppm

 

Scale Factor Temperature Sensitivity

20ppm/℃

 

Range Indicators

Input Range

±20g

 

Characteristics

Environmental Performance

Operating Temperature

-40℃~60℃

 

Storage Temperature

-45℃~70℃

 

General Requirements

Power Supply

18~36V(DC)

 

Stable Power Consumption

≤8W

Startup Power Consumption ≤15W

Mounting Hole Diameter

4-Φ4.5mm

 

Dimensions(mm)

70.3×70.3×53

 

Weight

≤500g

 

 

III Electrical Interface Definition (J63A-242-015-261TH)

Pinout

Signal

Type

Description

Remark

1,2

+24V

Input

Power Input

+24V

3,4

GND

Input

5

RS422_TX1+

Output

RS422 Serial Port 1

 

6

RS422_TX1-

Output

IMU Raw Data

7

RS422_RX1+

Input

 

8

RS422_RX1-

Input

 

9

RS422_TX2+

Output

RS422 Serial Port 2

IMU synchronization signal

10

RS422_TX2-

Output

11

RS422_RX2+

Input

12

RS422_RX2-

Input

13

RS232_TX1

Output

RS232 Serial Port 3

 

14

RS232_RX1

Input

 

 

IV Structure Diagram

 

 


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