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Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output

    Buy cheap Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output from wholesalers
     
    Buy cheap Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output from wholesalers
    • Buy cheap Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output from wholesalers
    • Buy cheap Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output from wholesalers

    Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output

    Ask Lasest Price
    Brand Name : Firepower
    Model Number : INS200A
    Certification : CE
    Price : negotiable
    Payment Terms : L/C, T/T
    Supply Ability : 500/Month
    Delivery Time : 1 week for sample
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    Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output

    Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output

    Product Description

    INS200A integrated navigation system has built-in high-performance MEMS gyroscope and accelerometer, which can receive external GNSS data, realize multi-sensor fusion and integrated navigation algorithm, and have short-term inertial navigation capability when GNSS is invalid.

    The product has high reliability and strong environmental adaptability. By matching different
    software, the products can be widely used in the fields of tactical and industrial unmanned aerial vehicles, unmanned vehicles, unmanned ships, aviation guided bombs, intelligent ammunition, rockets, mobile communication, mapping, seeker and stable platform.

    Technical parameters


    Item
    Indicators


    Gyro

    channel
    Measuring range
    -500°/s ~+500°/s
    Resolution
    ≤0.01°/h
    Bias residual
    -0.02°/h ~+0.02°/h
    Random walk

    ≤0.007°/√h
    Bias stability at room temperature
    ≤0.04°/h(1σ, 10s)
    Bias stability at full
    temperature
    ≤0.06°/h(1σ, 10s)
    Normal-temperature
    Bias repeatability
    ≤0.04°/h(1σ)
    Bias repeatability at full
    temperature
    ≤0.06°/h(1σ )
    Scale factor nonlinearity
    ≤30ppm
    Scale factor repeatability
    ≤30ppm(1σ)
    Gyro start time
    ≤5s
    Gyro bandwidth
    >300Hz
    Installation error
    residual of three-axis
    gyroscope

    ≤10"

    Acceleration
    channel
    Measuring range
    -20g ~ +20g
    Bias stability at
    full temperature
    ≤50ug(1σ)
    Bias repeatability
    at full temperature
    ≤80ug(1σ)
    Add up the starting time
    ≤5s
    Triaxial addition installation error residual
    ≤10"
    Alignment accuracy
    Alignment
    accuracy
    North seeking time
    ≤5min
    Heading Angle Alignment Repeatability
    ≤0.08°/cosL
    Pitch Alignment Repeatability
    ≤0.005°
    Roll Angle Alignment Repeatability
    ≤0.005°
    North-seeking mode
    Optional
    Integrated navigation accuracy (satellite effective)
    Integrated navigation accuracy
    Accuracy of course
    angle measurement
    ≤0.06°
    Accuracy of pitch
    angle measurement
    ≤0.03°

    Roll angle measurement accuracy

    ≤0.03°
    Speed accuracy
    ≤0.03m/s
    Position accuracy
    ≤1.5m
    Position accuracy

    ≤2cm+1ppm
    Inertial navigation accuracy (invalid satellite)
    Integrated navigation accuracy
    Accuracy of course angle maintenance
    ≤0.06°/h
    Pitch Angle Holding Accuracy
    ≤0.03°/h
    Accuracy of roll angle maintenance
    ≤0.03°/h
    Pure inertial horizontal positioning accuracy
    ≤1.0 nautical mile H(5h)
    Position positioning accuracy of odometer integrated navigation
    ≤0.2% (mileage greater than 3 km)

    Detailed photo

    Factory Photo

    Payment & Shipping

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