Low Cost Inertial Measurement Unit (2)

Low cost Inertial Measurement Unit

ER-MIMU-17
1. Small size: 47×44×14mm;
2. Light weight: 40g;
3. Gyro bias instability: 1º/h (Allen variance).

Low cost Inertial Measurement Unit

Low Cost Inertial Measurement Unit (2)

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    Introduction

    Low cost Inertial Measurement Unit

    Introduction
    ER- MIMU-17 is a micromechanical technology (MEMS)-based inertial measurement unit (IMU). Built-in three-axis gyroscope and three-axis accelerometer to measure three-axis angular velocity and acceleration.

    The ER-MIMU-17 uses a high-quality, reliable MEMS accelerometer and gyroscope. It can be used for attitude measurements. The product uses high-performance MEMS inertial devices, which have high reliability and high robustness, and can accurately measure the angular velocity and acceleration information of moving carriers in harsh environments.

    Features
    Three-axis digital gyroscope:
    Dynamic measurement range: ±400º/s;
    Bias instability: 1º/h (Allen variance);
    Angle random walk: 0.25º/√h.
    Three-axis digital accelerometer:
    Dynamic measurement range: 30g;
    Bias instability: 10ug(Allen variance);
    Ensure accuracy over the full temperature range (-40°C~80°C): Built-in high-performance temperature calibration and compensation algorithm;
    Low power consumption: 2W
    Communication interface: 1 SPI

    Application
    Industrial instrumentation attitude measurement
    Robot attitude control
    Indoor people tracking, navigation, and tracking
    Platform stability and control
    Pipeline Inspection, exploration & positioning

    Specifications

    Parameter Test condition Min value Typical value Max value Unit
    Gyroscope
    Measuring range ±400 º/s
    Bias stability 10s smoothing, 1σ 5 º/h
    Bias instability (1σ 25℃)Allen variance 1 º/h
    Random Walk <0.25 º/√h
    Bias Repeatability (1σ 25℃) 5 º/h
    Scale factor at 25°C 20000 LSB/°/s
    Scale factor non-linearity <200 ppm
    Scale factor repeatability 10 ppm
    Bandwidth 200 Hz
    Accelerometer
    Measuring range   ±30   g
    Bias instability Allen variance 10   ug
    Bias stability 10s smoothing, 1σ <50 ug
    Bias temp coefficient <20 ug/℃
    Bias Temp Hysteresis <1.5 mg
    Bias repeatability 100 ug
    Scale factor non-linearity <500 ppm
    Scale factor month repeatability <30 ppm
    Bandwidth 100 Hz
    Communication Interface
    1 way SPI Baud rate 15 MHz
    Electrical specification
    Voltage 6 12 V
    Power consumption 2 W
    Structural characteristics
    Dimension 47×44×14mm
    Weight 40 g
    Operating environment
    Operating temperature -40~80
    Storage temperature -55~105

    Dimension

    Dimension Of MEMS IMU


    Application Techniques

    1.IMU working principle & Tactical grade IMU product recommendations

    2.How Does an IMU Work?

    3.Choosing an IMU: FOG IMUs vs MEMS IMUs

    4.Application of IMU in the Field of Drones

    5.What is the Difference Between IMU and AHRS?

    6.How is IMU used?


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