Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation

Brand Name:Firepower
Certification:CE
Model Number:INS300
Minimum Order Quantity:1
Delivery Time:1 week for sample
Payment Terms:L/C, T/T
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Location: Shenzhen Guangdong China
Address: 429, Building A10, Fuhai Information Port, Xinhe Community, Fuhai Street, Shenzhen, Guangdong, China
Supplier`s last login times: within 22 hours
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Product Details

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


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 bandwidth>300HzDesign assurance, batch testing
Installation error residual of three-axis gyroscope≤10"


Acceleration channel
Measuring range-20g ~ +20gDesign 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"

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Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation

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