High Performance Navigation MEMS IMU

High Precision Navigation MEMS IMU

ER-MIMU-02 (0.05º/h) Features:
1. Measuring range ±400º/s;
2. Bias instability (Allan variance) 0.05º/h;
3. Light Weight.

High Precision Navigation MEMS IMU

High Performance Navigation MEMS IMU

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    High Performance Navigation MEMS IMU 02High Performance Navigation MEMS IMU 01High Performance Navigation MEMS IMU 03

    ER-MIMU-02 High Precision 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-MINU-02 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.

    Applications

    Construction machinery dip angle measurement, angle control, pylon operation monitoring, medical equipment angle control, satellite antenna star search, bridge, tall building, tower, dam monitoring and rock and soil monitoring, mining, attitude/heading reference system, integrated inertial navigation.

    Features

    Volume: 38.6 mm×44.8 mm×21.8 mm;

    5V power supply, low power consumption 1.0W;

    Lightweight: 50g;

    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.

    Specifications

    Gyro Parameter ER-MG2-300 ER-MG2-400 Unit
    Range ±300 ±400 deg/s
    Resolution 24 24 bits
    Data Rate 12K 12K Hz
    Group delay <5 <3 ms
    Bandwidth (-3dB) 50 100 Hz
    Scale Factor at 25°C 28000 20000 lsb/deg/s
    Scale Factor Repeatability (1σ) <50 <20 ppm
    Scale Factor VS Temperature (1σ) 300 100 ppm
    Scale Factor Non-Linearity (1σ) <300 100 ppm
    Bias Instability 0.03 0.05 deg/hr
    Bias stability 0.15 <0.5 deg/hr
    Bias stability 0.5 <1.5 deg/hr
    Angular Random Walk <0.01 <0.025 °/ √h
    Bias error over temperature (1σ) 10 3 deg/Hr
    Bias temperature variations, calibrated (1σ) <1 <0.5 deg/Hr
    Bias Run-Run(1σ) <0.3 <0.3 deg/hr
    Noise Peak to Peak ±0.010 ±0.05 deg/s
    G-Sensitivity <1 <1 °/hr/g
    VRE <1 <1 °/hr/g (rms)
    Startup Time 1 1 s
    Sensor Resonant Frequency 11K—13K
    Environment, Power and Physical
    Shock (operating) 500g,1ms, half sine wave
    Shock (survival) 10000g,1.0ms, half sine wave
    Vibration (Operating) 12grms,20Hz to 2KHz Random Vibration
    Operating Temperature -45°C—85°C
    Max storage (survival) Temperature -55°C—125°C
    Supply voltage 5±0.25V
    Current consumption 40mA
    Accelerometer Range 2-10 30-50 g
    Bandwidth 100 100 Hz
    Bias Stability (Allan Curve) <5 <10 ug
    Bias Stability (1s Standard Deviation)(1σ) <20 <50 ug
    Bias Month Repeatability 100-300 300-500 ug
    Bias Temp Coefficient <10 <50 ug/℃
    Bias Temp  Hysteresis <0.5 <1 mg
    Factor Scale Non-linearity <500 <1000 (2000@50g) ppm
    Factor Scale Month Repeatability <300 <300 ppm
    Factor Scale Temp Coefficient 10 10 ppm/℃
    ClassII Non-linearity Coefficient <100 <100 ug/g2
    Factor Scale 4000000-800000 200000-150000 Lsb/g
    Resolution 5 10 ug
    Start Time <1 <1 s
    Sampling Rate 1500 1500 Hz
    Shock(charged) 10000 10000 g
    Shock(uncharged) 10000 10000 g
    Vibration Rectification Error (6grms) / <0.4 mg/grms
    Operation Temp 70
    Voltage 5±0.25 5±0.25 V
    Current <15 <15 mA

    FAQ:

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

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