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High Precision Position INS Navigation System Sensor Output Pitch Roll Heading 3 Axis

Shenzhen Fire Power Control Technology Co., LTD
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    Buy cheap High Precision Position INS Navigation System Sensor Output Pitch Roll Heading 3 Axis from wholesalers
     
    Buy cheap High Precision Position INS Navigation System Sensor Output Pitch Roll Heading 3 Axis from wholesalers
    • Buy cheap High Precision Position INS Navigation System Sensor Output Pitch Roll Heading 3 Axis from wholesalers

    High Precision Position INS Navigation System Sensor Output Pitch Roll Heading 3 Axis

    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
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    High Precision Position INS Navigation System Sensor Output Pitch Roll Heading 3 Axis

    High-Precision Position And Navigation System Sensor Output Pitch, Roll Heading 3 Axis Acceleration 3 Axis Gyro Value


    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.


    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"

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