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Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance

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

    Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance

    Ask Lasest Price
    Brand Name : Firepower
    Model Number : INS300
    Certification : CE ROHS
    Price : negotiable
    Payment Terms : T/T
    Supply Ability : 500/month
    Delivery Time : 10 days
    • Product Details
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    Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance

    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.


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