FSU307 Fiber Optic Inertial Measurement Unit

FSU307 Fiber Optic Inertial Measurement Unit

Full-temp calibration
Harsh-environment resistant
Vibration & EMI resistant
Online upgrade & self-calib

Description
Key Features

 

  • Lightweight, domestic
  • Rich interfaces
  • 10 W low power
  • Full-temp calibration
  • Harsh-environment resistant
  • Vibration & EMI resistant
  • Online upgrade & self-calib
product-457-457

 

Applications

 

  • Mobile survey & attitude
  • Unmanned systems (ground/marine/UW)
  • Surveying & north-finding
  • Stabilized platforms
  • SATCOM-on-the-move
  • Autonomous driving & munitions

 

Product Introduction

 

Company's FSU307 fiber optic inertial measurement unit is a high-reliability, cost-effective navigation system for aircraft, UGVs, USVs, UAVs, and similar platforms. Inheriting a modular design philosophy, it integrates high-precision silicon photonic gyroscopes and MEMS accelerometers. Beyond IMU applications, its software is configurable for transfer alignment, integrated navigation, pure INS, and AHRS modes, adapting to diverse inertial navigation requirements to meet varied user needs.

 

Unique Technology

 

Company is a high-tech enterprise with full closed-loop capabilities from fiber winding equipment and coils to FOGs, fiber/MEMS inertial products, IMU circuits, software, and test equipment. End-to-end process control improves quality and reduces costs. Operating under ISO9001 with strict processes, it ensures product reliability and consistency.

 

FSU307 Fiber Inertial Measurement Unit Performance Specifications

 

Parameter

Specifications

Fiber OpticGyro

Range (°/s)

±500

Bias (°/h)

1

Bias Stability (°/h, 10s avg.)

0.5

Bias Instability (°/h, Allan)

0.05

Bias Repeatability (°/h, 6 cycles)

0.5

ARW (°/√h)

0.025

Scale Nonlinearity (ppm)

100

Cross-Coupling (rad)

≤0.001

Bandwidth (Hz)

≥200

MEMSAccelerometer

Range (g)

±30

FT Bias (mg, 3σ)

≤0.5

Bias Stability (μg, 10s avg.)

≤10

Bias Instability (μg, Allan, typ.)

≤3

Bias Repeatability (μg)

≤10

Velocity Random Walk (m/s/√h)

≤0.01

Scale Nonlinearity (ppm, ±1g)

≤100

Cross-Coupling (rad)

≤0.001

Bandwidth (Hz)

≥200

Electrical/Mechanical Interface

Input Voltage (V DC)

5

Power Consumption (W)

≤10

Dimensions (mm)

88.9×89.55

Unit Weight (kg)

≤0.5

Operating Environment

Operating Temperature (°C)

-40 ~ +70

Storage Temperature (°C)

-55 ~ +85

Vibration (g)

6 @ 20~2000 Hz

Shock (g)

100 , 11 ms

Reliability/Suitability

MTBF/MTTR (h)

10000 / 0.5

Maintenance

BIT 95%

 

Mechanical Dimensions Diagram

 

product-1238-827

 

Device Description

 

Product Overview

FSU307 fiber optic IMU is a high-reliability, cost-effective navigation system widely used in navigation, control, and measurement for aircraft, UGVs, USVs, and UAVs.

The IMU inherits a modular design philosophy, employing high-precision silicon photonic gyroscopes and high-precision MEMS accelerometers. Beyond standalone IMU operation, it supports configurable software modes including transfer alignment, integrated navigation, pure INS computation, and AHRS to maximize compatibility with diverse applications.

 

Product Composition

FSU307 fiber optic IMU consists of a three-axis silicon photonic gyroscope, high-precision MEMS accelerometer, signal processing circuit, navigation software, mechanical components, and test cable. Key components:

Table 1 IMU Main Components

No.

CompositionComponent

Qty

Model

Remarks

1

High-Precision INS

1

FSU307

 

2

Connector Plug

1

J20JD-21TJL

Male

 

Key Features

  • Key features of FSU307 fiber optic IMU:
  • Domestic core components, high performance, modular, lightweight
  • Rich interfaces
  • 10 W steady-state power
  • Full-temp calibration, -40°C to +70°C
  • Mechanical environment resistant
  • Vibration, shock, and EMI resistant
  • Online firmware upgrade and installation error compensation

 

Applications

  • Primary applications of FSU307 fiber optic IMU:
  • Mobile position and attitude reference
  • UGVs, USVs/UUVs
  • Surveying
  • Stabilized platforms
  • Underwater vehicles
  • SATCOM on the move
  • Intelligent driving
  • Munition guidance
  • Intelligent mining north-finding

 

Technical Parameters

 

System Specifications

Table 2 FSU307 Fiber Optic IMU Performance Specifications

Fiber Optic Gyroscope

Range (°/s)

±500

Bias (°/h)

1

Bias Stability (°/h, 10s avg.)

0.5

Bias Instability (°/h, Allan)

0.05

Bias Repeatability (°/h, 6 cycles)

0.5

ARW (°/√h)

0.025

Scale Nonlinearity (ppm)

100

Cross-Coupling (rad)

≤0.001

Bandwidth (Hz)

≥200

MEMS Accelerometer

Range (g)

±30

FT Bias (mg,3σ)

≤0.5

Bias Stability (μg,10savg.)

≤10

Bias Instability (μg,allan,typ)

≤3

Bias Repeatability (ug)

≤10

VRW (m/s/√h)

≤0.01

Scale Nonlinearity (ppm,±1g)

≤100

Cross-Coupling (rad)

≤0.001

Bandwidth (Hz)

≥200Hz

Electrical/Mechanical Interface

Input Voltage (V DC)

5

Power Consumption (W)

≤10

Dimensions (mm)

88.9×89.55

Unit Weight (kg)

≤0.5

Operating Environment

Operating Temperature (°C)

-40~ +70

Storage Temperature (°C)

-55~ +85

Vibration ( g)

6 @ 20~2000 Hz

Shock (g)

100 , 11 ms

Reliability/Suitability

MTBF/MTTR (h)

10000 / 0.5

Maintenance

BIT 95%

 

Mechanical Interface

Mechanical interface of FSU307 fiber optic IMU is shown below:

product-1238-827

Fig. 1 FSU307 Fiber Optic Inertial Measurement UnitMechanical InterfaceFig.

 

Electrical Interface

FSU307 IMU uses a J30JM-21ZKP connector, mating with J30J-21TJL plug. The connector pinout is defined as follows:

Table 3 FSU307 Fiber Optic IMU Connector Pinout

Pin

PinDefinition

DB9 Definition

Interface

FunctionDescription

1

Vin+

Red AlligatorVin+

Input Range+5V

System Power Input

12

2

GND

Black Alligator GND

GND

System Power Ground

13

4

Reserved

/

/

 

15

Reserved

/

16

RS422_RX+

DB9-M1-1

M1:Isolated RS422

Data output, system configUpgrade

5

RS422_RX-

DB9-M1-2

6

RS422_TX+

DB9-M1-3

17

RS422_TX-

DB9-M1-4

14

GGND

DB9-M1-5

7

Reserved

     

19

Reserved

 

18

Reserved

 

21

RS232_TXD2

DB9-M3-2

M3: Isolated RS232

NavigationData output

9

RS232_RXD2

DB9-M3-3

10

GGND

DB9-M3-5

8

PPS_IN

Pigtail

 

TTL Level

11

GGND

Pigtail

GND

Isolated Ground

20

TOV_OUT

Pigtail

   

3

GGND

Pigtail

GND

Isolated Ground

 

Data Protocol

 

The general IMU protocol outputs data in timed broadcast mode at 200 Hz, 40 bytes per frame, 460800 bps, 1 start bit, 8 data bits, 1 stop bit, no parity, LSB first. Baud rate and output rate are configurable.

Table 4 FSU307 Fiber Optic IMU Protocol

No.

Offset

Byte Count

Content

Scale

Range

Unit

Remarks

1

0

1

0x55

1

 

 

Header

2

1

1

0xAA

1

 

 

Header

3

2

1

36

1

 

 

Data Length

4

3

4

PCnum

1

 

 

1 ms Counter

5

7

4

Angular Rate X

0.000001

[-1000,1000]

°/s

 

6

11

4

Angular Rate Y

0.000001

[-1000,1000]

°/s

 

7

15

4

Angular Rate Z

0.000001

[-1000,1000]

°/s

 

8

19

4

Accel X

0.000001

[-40g,40g]

m/s2

 

9

23

4

Accel Y

0.000001

[-40g,40g]

m/s2

 

10

27

4

Accel Z

0.000001

[-40g,40g]

m/s2

 

11

31

2

Temperature

0.008

[-120,120]

℃

 

12

33

2

Reserved

 

 

 

 

13

35

4

Reserved

 

 

 

 

14

39

1

Checksum

1

[0, 255]

 

Lower 8 bits of bytes 2-38 sum

 

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