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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

Brand Name : Firepower

Model Number : INS300

Certification : CE ROHS

Place of Origin : CHINA

MOQ : 1

Price : negotiable

Payment Terms : T/T

Supply Ability : 500/month

Delivery Time : 10 days

Packaging Details : sponge+carton

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）

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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


Product Tags:

3 Axis INS Navigation System

      

GNSS 3 Axis Gyro

      

CE 3 Axis Gyro

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

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