Low Cost Mems Imu

Low Cost MEMS IMU

ER-MIMU-M01C(≤4°/h)
1. Miniaturized MEMS IMU;
2. Low power consumption;
3. Low price;
4. Full temperature compensation.

Low Cost MEMS IMU

Low Cost Mems Imu

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    Introduction

    ER-MIMU-M01C Low Cost MEMS IMU

    Introduction
    The ER-MIMU-M01C Low Cost MEMS IMU is a general-purpose, miniaturized, low-priced inertial component that contains three-axis gyroscope and three-axis accelerometer information. Temperature compensation is performed through the bias stability and scale of each axis to improve its measurement accuracy.

    Features
    Miniaturized IMU
    Low power consumption
    Low price
    Full temperature compensation
    Gyro bias instability: ≤4°/h
    Gyro bias stability (1σ): ≤15°/h
    Accelerometer  bias instability: ≤0.04mg

    Application 
    Inertial navigation: combined navigation, platform stability
    Attitude control: UAV
    Automotive field: unmanned, electronic stability program

    Specifications

    Gyroscope
    Measuring range ±450°/s
    Full temperature bias ≤180°/h
    Angular random walk ≤0.3°/ √h
    Bias instability ≤4°/h
    Bias stability (1σ) ≤15°/h
    Bias repeatability (1σ) ≤15°/h
    Scale factor non-linearity ≤100ppm
    Bandwidth (10~250Hz adjustable) 150Hz
    Accelerometer
    Measuring range ±10g
    Full temperature bias ≤6mg
    Rate random walk ≤0.03m/s/√h
    Bias instability ≤0.04mg
    Bias stability (1σ) ≤0.3mg
    Bias repeatability (1σ) ≤0.3mg
    Scale factor non-linearity (±1g) ≤300ppm
    Bandwidth (10~250Hz adjustable) 150Hz
    System
    Supply voltage 5V±0.3V
    Operating temperature range -45℃~+85℃
    Shock resistance ≥2000g
    Vibration ≥20grms
    Size 23.7mm×23.7mm×9.9mm
    Weight ≤25g
    Interface type(--) UART
    Connector(--) Molex 5015680607
    Output interface wiring definition
    VCC(+5V) Power supply positive
    GND Power supply ground
    TXD receive
    RXD receive
    PPS synchronization
    - -

    Dimensions

    Dimension Of Low Cost Mems Imu


    Application Techniques

    1.IMU and GPS fusion algorithm principle

    2.MEMS IMU error analysis and compensation

    3.Reusable spacecraft IMU dynamic accuracy assessment method

    4.Research on MEMS IMU error modeling and temperature compensation technology

    5.Calibration method and error analysis of low-precision MEMS IMU

    6.MEMS-IMU error calibration compensation method that does not rely on precision turntable


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