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 (Allan variance).

Low cost Inertial Measurement Unit

Low Cost Inertial Measurement Unit (2)

Get Price Now



    Share to:

    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 (Allan variance);
    Angle random walk: 0.25º/√h.
    Three-axis digital accelerometer:
    Dynamic measurement range: 30g;
    Bias instability: 10ug(Allan 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 A B Unit
    Gyroscope
    Measuring range   ±400 ±400 º/s
    Bias stability 10s smoothing, 1σ 5 4 º/h
    Bias instability (1σ 25℃)

    Allan variance

    1 1 º/h
    Random Walk   0.25 0.2 º/√h
    Bias Repeatability (1σ 25℃) 5 4 º/h
    Scale factor at 25°C   20000 20000 LSB/°/s
    Scale factor non-linearity   200 200 ppm
    Bandwidth   200 200 Hz
    Accelerometer
    Measuring range   ±30 g
    Bias instability Allan 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?


    More Products

    North Seeking Mems Imu For Gyro Tools
    North-Seeking MEMS IMU for Gyro Tools
    High Performance Navigation MEMS IMU
    High Performance Navigation MEMS IMU
    High Performance Mems Imu
    High Performance MEMS IMU
    High Precision Navigation MEMS IMU
    High Precision Navigation MEMS IMU
    North Seeking Mems Imu For Gyro Tools
    Low Power Inertial Measurement Unit
    High Precision Stable-Control MEMS IMU
    Ask for a Quote



      Menu