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Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation

Shenzhen Fire Power Control Technology Co., LTD
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    Buy cheap Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation from wholesalers
     
    Buy cheap Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation from wholesalers
    • Buy cheap Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation from wholesalers
    • Buy cheap Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation from wholesalers

    Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation

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    Brand Name : Firepower
    Model Number : INS300
    Certification : CE
    Price : negotiable
    Payment Terms : L/C, T/T
    Supply Ability : 500/Month
    Delivery Time : 1 week for sample
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    Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation

    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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