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Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance

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Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance

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

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"
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.

Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance


Product Tags:

FOG INS Navigation System

      

Nine Axis Output Navigation System

      

Airplane Inertial Navigation System

      
China Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance wholesale

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