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High Precision Position INS Navigation System Sensor Output Pitch Roll Heading 3 Axis

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High Precision Position INS Navigation System Sensor Output Pitch Roll Heading 3 Axis
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Features
Specifications
Product: FOG INS
Gyro Range: 500°/s
Gyro Resolution: ≤0.01°/h
Gyro Bias: ±0.02°/h
Gyro Bias Stability: ≤0.01°/h(1σ)
Accelerometer Range: ±20g
Zero Bias Stability: ≤80ug(1σ)
Zero-bias Repeatability: ≤80ug(1σ)
High Light:

3 Axis INS Navigation System

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GNSS 3 Axis Gyro

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CE 3 Axis Gyro

Basic Infomation
Place of Origin: CHINA
Brand Name: avic
Certification: CE ROHS
Model Number: INS300
Payment & Shipping Terms
Packaging Details: sponge+carton
Delivery Time: 10 days
Payment Terms: T/T
Supply Ability: 500/month
Product Description

High-Precision Position And Navigation System Sensor Output Pitch, Roll Heading 3 Axis Acceleration 3 Axis Gyro Value

 

INS-300 is a high-precision integrated navigation system independently developed by Avic group. It contains three self-developed 98 fiber optic gyroscopes, three quartz accelerometers, high-precision sampling circuit, navigation computer circuit, GNSS module and power supply 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.

 

Gyro specs

 

 

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"  
 
 

acc specs

 

Project Indicators Remark

 

 

Acceleration channel

Measuring range -20g ~ +20g Design and selection guarantee
Zero bias stability at full temperature ≤80ug(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"  
 
 

High Precision Position INS Navigation System Sensor Output Pitch Roll Heading 3 Axis 0

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