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Anti-interference Three Axis IMU Gyro for Inertial navigation

Shenzhen Fire Power Control Technology Co., LTD
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    Buy cheap Anti-interference Three Axis IMU Gyro for Inertial navigation from wholesalers
     
    Buy cheap Anti-interference Three Axis IMU Gyro for Inertial navigation from wholesalers
    • Buy cheap Anti-interference Three Axis IMU Gyro for Inertial navigation from wholesalers

    Anti-interference Three Axis IMU Gyro for Inertial navigation

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    Brand Name : Firepower
    Model Number : GI200-A0-IMU
    Certification : CE
    Price : negotiable
    Payment Terms : T/T
    Supply Ability : 1000/month
    Delivery Time : 1 week
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    Anti-interference Three Axis IMU Gyro for Inertial navigation

    Anti-interference Three Axis IMU Gyro for Inertial navigation


    Product Description


    The GI200-A0 (B0) -IMU is an inertial measurement unit (IMU) based on micromachining technology (MEMS), with built-in high-performance MEMS gyroscope and MEMS accelerometer, outputting 3 angular velocities and 3 accelerations.

    GI200-A0 (B0) -IMU features high reliability and strong environmental adaptability. By matching different software, the product can be widely used in intelligent driving, tactical and industrial UAV, intelligent ammunition, seeker, mobile communication, mapping, stable platform and other fields.

    The GI200-A0 (B0) -IMU is available in A0 (low configuration) and B0 (high configuration) versions.


    Main Features

    1. Three-axis digital gyroscope:
      1. ± 2000º/s dynamic measurement range;
      2. A0 bias stability: 6 °/H (GJB, 10s, Z-axis), 9 °/H (GJB, 1s, Z-axis), 1.6 °/H (ALLAN, Z-axis);
      3. B0 bias stability: 3 °/H (GJB, 10s, Z-axis), 4.5 °/H (GJB, 1s, Z-axis), 0.8 °/H (ALLAN, Z-axis);
    2. Triaxial digital accelerometer:
      1. ± 200g dynamic measuring range;
      2. A0 bias stability: 0.4mg (GJB, 10s), 0.6mg (GJB, 1s), 0.06 mg (ALLAN);
      3. B0 bias stability: 0.2mg (GJB, 10s), 0.3mg (GJB, 1s), 0.03mg (ALLAN);
    3. High reliability: MTBF > 20000h;
    4. Guaranteed accuracy within the full temperature range (-40 ℃ ~ 80 ℃): built-in high-performance temperature calibration and compensation algorithm;
    5. Suitable for working under strong vibration conditions;
    6. Interface 1 channel UART, 1 channel SPI, 1 channel CAN

    Main Application Field

    • Intelligent driving
    • Tactical and Industrial UAV
    • Smart Munitions
    • Seeker
    • Communication in motion
    • Mapping
    • Stabilize the platform

    Product Indicators


    ParameterTest conditionsMinimum valueTypical valueMaximum valueUnit
    GyroDynamic measuring range  5002000º/s
    Zero bias stabilityAllan variance, Z-axis 1.6 º/h
    Allan variance, X and Y axis 3.2 º/h
    10 s average (-40 ℃ ~ + 80 ℃, constant temperature), Z-axis 6 º/h
    1s average (-40 ℃ ~ + 80 ℃, constant temperature), Z-axis 9 º/h
    10 s average (-40 ℃ ~ + 80 ℃, constant temperature), X axis and Y axis 12 º/h
    1 s average (-40 ℃ ~ + 80 ℃, constant temperature), X axis and Y axis 18 º/h
    Zero biasZero-bias range, Z-axis ±0.14 º/s
    Zero-bias range, X-axis and Y-axis ±0.4 º/s
    Zero bias change over full temperature range, Z-axis① ±0.04 º/s
    Zero bias change over full temperature range, X and Y axis① ±0.12 º/s
    Successive Start Repeatability, Z-axis 0.004 º/s
    Successive Start Repeatability, X-Axis and Y-Axis 0.012 º/s
    Day-by-day start repeatability, Z-axis 0.006 º/s
    Start repetition day by day, X axis and Y axis 0.018 º/s
    Ffect of linear acceleration on bias 0.004 º/s/g
    Influence of vibration on zero bias, change before and after vibration② 0.004 º/s/g
    Influence of vibration on zero bias, change before and during vibration② 0.004 º/s/g
    Scale factorScale factor accuracy, Z-axis 0.6 %
    Scale Factor Accuracy, X and Y Axis 1.2 %
    Scale factor nonlinearity, Z-axis 0.02 %FS
    Scale Factor Nonlinearity, X and Y Axis 0.04 %FS
    Angular random walk  0.3 °/√hr
    Noise density  0.002 °/s/√Hz
    Resolution  3.052×107 º/s/LSB
    Bandwidth  200 Hz
    AccelerometerDynamic measuring range  16200g
    Zero bias stabilityAllan variance 0.06 mg
    10 s average (-40 ℃ ~ + 80 ℃, constant temperature) 0.4 mg
    1s average (-40 ℃ ~ + 80 ℃, constant temperature) 0.6 mg
    Zero biasZero bias range 1630mg
    Zero bias change in full temperature range, peak-to-peak value① 1020mg
    Repeatability of successive starts 1 mg
    Repeatability is initiated on a daily basis 1.6 mg
    Zero-bias temperature coefficient 0.10.2mg/℃
    Scale factorScale factor accuracy 4 %
    Scale factor nonlinearity 0.2 %FS
    Speed random walk  0.058 m/s/√hr
    Noise density  0.05 mg/√Hz
    Resolution  1.221×108 g/LSB
    Bandwidth  200 Hz
    MagnetometerMagnetic field rangeBrg,xy ±1300 μT
    Brg,z ±2500 μT
    Resolution  0.3 μT
    Heading and longitude30 μT horizontal geomagnetic component, 25 ℃ ±2.5 deg
    Communication interface1-channel SPIBaud rate  15MHz
    1-channel UARTBaud rate 230.4 Kbps
    1- channel CANBaud rate  1MHz
    Sampling frequencySPI 2001000Hz
    UART 200 Hz
    CAN 200  
    Electrical characteristicsVoltage 33.33.6V
    Power consumption   1.5W
    RippleP-P  100mV
    Structural characteristicsSize  47×44×14 mm
    Weight  50 g
    Use environmentOperating temperature -40 80
    Storage temperature -45 85
    Vibration  20~2000Hz,6.06g  
    Impact  1000g,0.5ms  
    ReliabilityMTBF  20000 h
    Continuous working time  120 h
    1: Calculate the zero deviation of the whole temperature change process, the temperature change rate is ≤ 1 ℃/min, and the temperature range is -40 ℃ ~ + 80 ℃;
    2: Vibration condition is 6.06 G, 20Hz ~ 2000Hz

    Product Structure


    Anti-interference Three Axis IMU Gyro for Inertial navigation

    L47mm x W44mm x H14mm(L x W x H)


    Electrical interface


    Anti-interference Three Axis IMU Gyro for Inertial navigation

    Anti-interference Three Axis IMU Gyro for Inertial navigation

    Quality Anti-interference Three Axis IMU Gyro for Inertial navigation for sale
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