High Precision Stable-control MEMS IMU

High Precision Stable-control MEMS IMU

ER-MIMU-03 (<0.3º/h) Features:
1. Measuring range ±400º/s;
2. Bias instability (Allan variance) <0.3º/h;
3. Bias (Full Temp) <9°/h.

High Precision Stable-control MEMS IMU

High Precision Stable-control MEMS IMU

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    High Precision Stable-control MEMS IMUHigh Performance Navigation MEMS IMUHigh Precision Stable-control MEMS IMU

    ER-MIMU-03 High Precision Stable-control MEMS IMU

    Inertial Measurement Unit, referred to as IMU, is a device to measure the attitude angle (or angular velocity) and acceleration of the three axis of the object. Gyroscope and accelerometer are the core devices of inertial navigation system (INS). With the built-in accelerometer sensor and gyroscope, the IMU can measure the linear acceleration and rotation angular velocity from three directions and can obtain the attitude, velocity and displacement information of the carrier through the resolving.

    ER-MIMU-03 uses MEMS accelerometer and gyroscope with high quality and reliability, RS422 and external communication, baud rate can be flexibly set between 9600~921600, through the communication protocol to set the user’s required communication baud rate. With X, Y, Z three-axis precision gyro, X, Y, Z three-axis accelerometer with high resolution, can be output by RS422 X, Y, Z three axis of gyroscope and accelerometer’s original hexadecimal complement data (including gyro hexadecimal complement the numerical temperature, angle, the accelerometer hexadecimal temperature, the acceleration hexadecimal complement number); It can also output float dimensionless values of the gyroscope and accelerometer processed by the underlying calculation.


    General Aviation / Flight Control

    AHRS (Attitude Heading Reference System)

    GPS-aided Navigation

    Autonomous and Remotely Operated Vehicles



    Volume: 44.84 mm×38.88 mm×21.39 mm;

    5V power supply, low power consumption 1.0W;

    Light weight: ≤60g;

    Products include X, Y, Z three axis MEMS gyro and X, Y, Z three axis MEMS accelerometer;

    RS422 bus communication, baud rate from 9600~921600 can be set.


    Item Parameter Unit
    Gyro Performance
    Range ±400 °/s
    Bandwidth (-3dB) 250 Hz
    Scale Factor at 25°C 16000 lsb/deg/s
    Scale Factor Repeatability (1σ) <50 ppm
    Scale Factor VS Temperature (1σ) 300 ppm
    Scale Factor Non-Linearity (1σ) <300 ppm
    Bias Instability <0.3° °/hr
    Bias stability (10s 1σ) <3 °/hr
    Bias stability (1s 1σ) <9 °/hr
    Bias Run-Run (1σ) <1 °/hr
    Accelerometer Performance
    Range 10-30 30-50 g
    Bandwidth 100 100 Hz
    Bias Stability (10s,1σ) <30 <50 μg
    Bias Repeatability 200-500 500-700 μg
    Bias Temp Coefficient <20 <50 μg/℃
    Bias Temp Hysteresis <0.5 <1 mg
    Factor Scale Non-linearity <500 <1000 ppm
    Factor Scale Repeatability <300 <300 ppm
    Factor Scale Temp Coefficient 10 10 ppm/℃
    Class II Non-linearity Coefficient <100 <100 μg/g²
    Factor Scale 4-8*106 1.5-2*105  Lsb/g
    System Performance
    Supply Voltage 5V
    Supply Consumption 1W
    Interface RS422
    Vibration 6.06g (10~2000Hz)
    Shock 5000g, 0.1ms
    Operate Temp -45℃~+ 85℃
    Storage Temp -55℃~+ 105℃
    Weight ≤60g
    Size 44.84 mm×38.88 mm×21.39 mm
    All values typical at +25,+12Vdc unless otherwise statement


    1. What are the quotation methods?

    If you have DHL or Fedex account, we can quote EXW price, otherwise CIF or FOB price.

    2. Are there any discounts?

    After we submit the sample price, if more quantity is needed, we will quote the bulk price.

    3. How long will it take to deliver the goods after placing the order?

    For sensors, parts and modules: in stock-one week; no stock-2-4 weeks; For systems, generally, 8-12 weeks.

    4. How to deal with the quality problems?

    After confirming that the product has quality problems, we will replace it for you free of charge in the shortest possible time.

    If interested in High Precision Stable-control MEMS IMU, pls contact us: info@ericcointernational.com

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