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Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation

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Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation

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Brand Name : Firepower

Model Number : INS300

Certification : CE

Place of Origin : CHINA

MOQ : 1

Price : negotiable

Payment Terms : L/C, T/T

Supply Ability : 500/Month

Delivery Time : 1 week for sample

Packaging Details : Wooden Box

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

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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"


Product Tags:

Unmanned Ship Inertial Navigation System

      

Fiber Optic Inertial Navigation System

      

Integrated Inertial Navigation System

      
Cheap Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation for sale

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