Low-cost Attitude-control MEMS IMU

High Performance Navigation MEMS IMU

1. 3 axis gyroscope & 3-axis accelerometer;
2. High performance and small size;
3. Gyro bias instability: 0.05 deg/hr.

High Performance Navigation MEMS IMU

Low-cost Attitude-control MEMS IMU

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    Low-cost Attitude-control MEMS IMULow-cost Attitude-control MEMS IMULow-cost Attitude-control MEMS IMU

    High Performance Navigation 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-06 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.

    Application areas

    Antenna and Line of Sight Stabilization Systems

    Integrated Navigation Systems & Inertial Guidance System

    Flight Control & Guidance System

    Attitude Heading Reference Systems (AHRS)

    Stabilization of Antennas, Cameras & Platforms

    Aerial and Marine Geo-mapping / Surveying

    Performance indicators

    Item Parameter Unit
    Gyro performance
    Range 400 deg/s
    Bandwidth (-3dB) 100 Hz
    Scale Factor at 25°C 20000 lsb/deg/s
    Scale Factor Repeatability (1σ) <20 ppm
    Scale Factor VS Temperature (1σ) 100 ppm
    Scale Factor Non-Linearity (1σ) 100 ppm
    Bias Instability 0.05 deg/hr
    Bias stability (10s 1σ) <0.5 deg/hr
    Angular Random Walk <0.025 °/ √h
    Bias error over temperature (1σ) 3 deg/Hr
    Bias temperature variations, calibrated (1σ) <0.5 deg/Hr
    Bias Repeatability (1σ) <0.3 deg/hr
    Accelerometer performance
    Range 10-30 30-50 g
    Bandwidth 100 100 Hz
    Bias Stability (1s) (1σ) <30 <50 ug
    Bias Repeatability 200-500 300-500 ug
    Bias Temp Coefficient <20 <50 ug/℃
    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 ug/g2
    Factor Scale 4000000-800000 200000-150000 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 ≤50g
    Size 43.2mm×43.2mm×35mm


    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 Performance Navigation MEMS IMU, pls contact us: info@ericcointernational.com

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