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Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output

Shenzhen Fire Power Control Technology Co., LTD
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    Buy cheap Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output from wholesalers
     
    Buy cheap Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output from wholesalers
    • Buy cheap Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output from wholesalers
    • Buy cheap Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output from wholesalers
    • Buy cheap Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output from wholesalers
    • Buy cheap Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output from wholesalers
    • Buy cheap Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output from wholesalers

    Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output

    Ask Lasest Price
    Brand Name : Firepower
    Model Number : IMU6-1
    Price : 2000$
    Payment Terms : L/C,D/A,D/P,T/T,Western Union
    Supply Ability : 500/month
    Delivery Time : 1 Week for sample
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    Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output

    Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output
    Key Specifications
    AttributeValue
    Gyro Measuring range±400°/s
    Bias Stability0.3°/h
    Angular Random Walk0.15º/√h
    Bias repeatability (1σ)1°/h
    Scale Factor Repeatability (1σ)150ppm
    3 dB Bandwidth250Hz
    Accelerometer bias stability0.02mg
    Weight55g
    Misalignment±0.05°
    Power consumption2W
    Product Overview

    The IMU6 MEMS Inertial Measurement Unit is a highly integrated sensing system that combines:

    • Three-axis gyroscope
    • Three-axis accelerometer
    • Three-axis inclination angle sensor
    • Temperature sensor
    • Signal processing board
    • Mechanical housing
    • Accompanying software

    Designed to measure three-axis angular rate, linear acceleration, and inclination angle of moving platforms, the system features comprehensive error compensation including temperature compensation, installation misalignment correction, and nonlinear compensation.

    Outputs high-accuracy data via standard RS-422 serial interface following predefined communication protocol.

    Technical Specifications
    Gyroscope Specifications
    ParameterUnitIMU6-1IMU6-1AIMU6-1BIMU6-1C
    Measuring range (customizable)°/s±400±400±400±2000
    In-Run Bias Stability(@ Allan variance)°/h0.30.10.051
    Bias stability @10s (10s smooth, 1σ, room temperature)°/h310.56
    Bias stability in full temperature°/h103218
    Angular Random Walk°/√h0.150.10.020.3
    Bias repeatability (1σ)°/h10.50.32
    Bias acceleration sensitivity°/h/g1112
    Scale Factor Non-Linearity(1σ)ppm150150150300
    Scale Factor Repeatability (1σ)ppm202020100
    Misalignment°±0.05±0.05±0.05±0.05
    3 dB BandwidthHz250200150250
    Accelerometer Technical Indicators
    ParameterUnitIMU6-1y-1IMU6-1y-2IMU6-1y-3IMU6-1y-4
    Measuring range (customizable)g±10±30±50±80
    In-Run Bias Stability (Allan Variance @ 25 ℃)mg0.020.050.10.2
    Bias stability @10smg0.050.20.51
    Bias stability in full temperaturemg13515
    Angular Random Walkm/s/√h0.0010.0020.0050.01
    Bias repeatability(1σ)mg0.10.512
    Scale Factor Repeatability (1σ)ppm200200200200
    Scale Factor Non-Linearity(1σ)ppm50100200300
    Misalignment°±0.05±0.05±0.05±0.05
    3 dB BandwidthHz100100100100
    Tilt Angle Specification (Optional)
    ParameterUnitIMU6-1y-x
    Measuring range (customizable)g±1.7
    Bias stability (1s smoothing)mg0.5
    Random walkm/s/√h0.08
    Scale factor non-linearityppm100
    Electrical Characteristics
    ParameterUnitIMU6-1y-x
    VoltageV5
    Power consumptionW2
    RipplemV100
    Environmental Adaptability
    ParameterUnitIMU6-1y-x
    Operating temperature-45~85
    Storage temperature-55~105
    Vibration--10~2000Hz,6.06g
    Impact--1000g,0.1ms
    Weightg55±5
    Outline Structure
    IMU6 Inertial Measurement Unit outline structure diagram
    Quality Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output for sale
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