• Advanced Fiber Optic Gyro Gnss/Ins Integrated Inertial Navigation System
  • Advanced Fiber Optic Gyro Gnss/Ins Integrated Inertial Navigation System
  • Advanced Fiber Optic Gyro Gnss/Ins Integrated Inertial Navigation System

Advanced Fiber Optic Gyro Gnss/Ins Integrated Inertial Navigation System

Type: Inertial Navigation
Output Signal Type: Digital Output
Measuring Shaft Quantities: Three
Accuracy Grade: 0.008deg/H
IP Rating: IP67
Certification: CE
Customization:
Gold Member Since 2023

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  • Overview
  • Product Description
  • Detailed Photos
  • Product Parameters
  • Company Profile
Overview

Basic Info.

Model NO.
INS300
Customized
Customized
Gyro Range
-500deg/S~-500deg/S
Acceleration Range
20g
Heading Accuracy
0.06deg
Pitch & Roll Accuracy
0.005deg
Transport Package
Sponge and Box
Specification
162*162mm
Trademark
AVIC
Origin
China
Production Capacity
100/Month

Product Description

Advanced fiber optic gyro GNSS/INS integrated inertial navigation system

Product Description

INS300 is a high-precision integrated navigation system independently developed by AVIC. It contains three self-developed 98 fiber optic gyroscopes, three quartz accelerometers, high-precision sampling circuit, navigation computer circuit, GNSS module and power circuit. And high-precision position and navigation in a complex environment are realized through multi-sensor fusion and an integrated navigation algorithm. The product has high reliability and strong environmental adaptability. The products can be widely used in intelligent driving, unmanned aerial vehicle, surveying and mapping, marine compass, stable platform, underwater vehicle, roadheader, mining machinery and other fields.

 

Detailed Photos

Advanced Fiber Optic Gyro Gnss/Ins Integrated Inertial Navigation System
Advanced Fiber Optic Gyro Gnss/Ins Integrated Inertial Navigation System

 

Product Parameters

Project Indicators  Remark



Gyro channel
Measuring range -500°/s ~+500°/s  
Resolution ≤0.01°/h  
Zero-bias residual -0.02°/h ~+0.02°/h  
Random walk ≤0.0015°/√h  
Zero bias stability at room temperature ≤0.01°/h(1σ,10s) 10 seconds smoothing, 1H test result
Zero bias stability at full temperature ≤0.015°/h(1σ,10s) 10 seconds smoothing, 1H test result
Normal-temperature zero-bias repeatability ≤0.01°/h(1σ) Statistics of 6 test data
Zero-bias repeatability at full temperature ≤0.015°/h(1σ) Take 2 zero-bias data at full temperature, high temperature, low temperature and normal temperature respectively
Scale factor nonlinearity ≤5ppm Full temperature and constant temperature
Scale factor repeatability ≤5ppm(1σ) Full temperature and constant temperature
  Gyro start time ≤5s  
  Gyro bandwidth >300Hz Design assurance, batch testing
  Installation error residual of three-axis gyroscope ≤10"  
 
Project Indicators  Remark


Acceleration channel
Measuring range -20g ~ +20g Design and selection guarantee
Zero bias stability at full temperature ≤50ug(1σ) 10 seconds smoothing, 1H test result
Zero-bias repeatability at full temperature ≤80ug(1σ) Take 2 zero-bias data at full temperature, high temperature, low temperature and normal temperature respectively
Add up the starting time ≤5s  
Triaxial addition installation error residual ≤10"  
 

Company Profile

Advanced Fiber Optic Gyro Gnss/Ins Integrated Inertial Navigation System

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Gold Member Since 2023

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Manufacturer/Factory, Trading Company
Registered Capital
1000000 RMB
Plant Area
1001~2000 square meters