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Shenzhen Fire Power Control Technology Co., LTD
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Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance

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Shenzhen Fire Power Control Technology Co., LTD

City: shenzhen

Province/State:guangdong

Country/Region:china

Tel:86-755-23097872

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Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance

Brand Name Firepower
Model Number INS300
Certification CE ROHS
Place of Origin CHINA
Minimum Order Quantity 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)
Detailed Product Description

Combined Navigation System Nine Axis Output For Airplan Ship Vehicle Navigation Guidance​

 

 

Gyro specs

 

 

ProjectIndicatorsRemark

 

 

 

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≤5ppmFull temperature and constant temperature
Scale factor repeatability≤5ppm(1σ)Full temperature and constant temperature
 Gyro start time≤5s 
 Gyro bandwidth300HzDesign assurance, batch testing
 Installation error residual of three-axis gyroscope≤10" 
 
 

acc specs

 

ProjectIndicatorsRemark

 

 

Acceleration channel

Measuring range-20g ~ +20gDesign 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" 
 
Introduction
 

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.

 

 

Product Tags: FOG INS Navigation System   Nine Axis Output Navigation System   Airplane Inertial Navigation System  
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