High Precision Navigation Mems Inertial Measurement Unit

High-Precision Navigation MEMS Inertial Measurement Unit

ER-MIMU-15
1. Small size: 47×44×14mm;
2. Light weight: 40g;
3. Gyro bias instability: 0.03-0.05 º/h (Allan variance).

High-Precision Navigation MEMS Inertial Measurement Unit

High Precision Navigation Mems Inertial Measurement Unit

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    Introduction

    ER-MIMU-15 High-Precision Navigation MEMS Inertial Measurement Unit

    Introduction
    ER- MIMU-15 is a MEMS inertial measurement unit with large dynamic measurement range and high accuracy, which has the advantages of small size and light weight. Built-in three-axis high-precision gyroscope and three-axis high-precision accelerometer for measuring three-axis angular velocity and acceleration.

    It can be used for precise navigation, control, and dynamic measurements. Even in harsh environments, angular velocity and acceleration information of moving carriers can be accurately measured.

    Features
    Three-axis digital gyroscope:
    Dynamic measurement range: ±400º/s;
    Bias instability: 0.05 º/h (Allan variance)
    Angular random walk: 0.025º/√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.

    Applications
    Line-of-sight stabilization system
    Integrated navigation system and inertial guidance system
    Flight control and guidance systems
    Attitude Heading Reference System (AHRS)
    Antenna, camera and platform stability
    Aerial and Marine geographic mapping/surveying

    Specifications

    Parameter Test condition A B Unit
    Gyroscope
    Measuring range   ±300 ±400 º/s
    Bias stability 10s smoothing, 1σ 0.15 <0.5 º/h
    Bias instability (1σ 25℃)

    Allan variance

    0.03 0.05 º/h
    Random Walk   <0.01 <0.025 º/√h
    Bias Repeatability (1σ 25℃) <0.3 <0.3 º/h
    Scale factor at 25°C   28000 20000 LSB/°/s
    Scale factor non-linearity <300 100 ppm
    Scale factor repeatability <50 <20 ppm
    Bandwidth (3dB)   50 100 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 High-Precision Navigation MEMS Inertial Measurement Unit


    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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