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products details

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Inertial Navigation System
Created with Pixso.

Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation

Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation

Brand Name: Firepower
Model Number: INS300
MOQ: 1
Price: negotiable
Payment Terms: L/C, T/T
Supply Ability: 500/Month
Detail Information
Place of Origin:
CHINA
Certification:
CE
Product Name:
Fiber Optic Inertial Navigation System
Gyro Range:
±500°/s
Gyro Zero Bias Stability:
±0.02°/h
Random Walk:
≤0.0015°/√h
Gyro Bandwidth:
>300Hz
Acc Range:
±20g
Acc Zero Bias Stability:
≤50ug
Scale Factor Nonlinearity:
≤5ppm
Packaging Details:
Wooden Box
Supply Ability:
500/Month
Highlight:

Unmanned Ship Inertial Navigation System

,

Fiber Optic Inertial Navigation System

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Integrated Inertial Navigation System

Product Description

Fiber Optic Integrated Inertial Navigation System for Unmanned Ship Navigation

 

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.

 

Main 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"  
     


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"