Low Cost Mems Imu

Low Cost Inertial Measurement Unit

ER-MIMU-M02A :
1.Gyro dynamic measurement range: ±450º/s;
2.Gyro bias instability: 0.3 º/h (Allen variance);
3.Gyro angle random walk: 0.15º/√h.
4.Accelerometer bias stability: 2ug (Allen variance)

Low Cost Inertial Measurement Unit

Low Cost Mems Imu

Get Price Now



    Share to:

    Introduction

    ER-MIMU-M02A  Low Cost Inertial Measurement Unit

    Introduction
    ER-MIMU-M02A is an inertial measurement unit (IMU) based on micro-mechanical technology (MEMS). It is a complete inertial system with a built-in three-axis gyroscope and a three-axis accelerometer to measure the three-axis angular parameters of the carrier, such as speed, acceleration, etc. The output data after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation, etc.) can be solved to obtain information such as carrier attitude, speed, displacement, etc. It also has a built-in three-axis magnetic sensor and air pressure sensor.

    Features
    Three-axis digital gyroscope:
    Dynamic measurement range: ±450º/s;
    Bias instability: 0.3 º/h (Allen variance);
    Angle random walk: 0.15º/√h.
    Three-axis digital accelerometer:
    Dynamic measurement range: ±20g;
    Bias stability: 2ug (Allen variance);
    Angular Random Walk: 0.005m/s√h;
    Ensure accuracy over the full temperature range (-40°C~80°C): Built-in high-performance temperature calibration and compensation algorithm;
    Communication interface: 1 SPI

    Application
    unmanned aerial vehicles, aerial photography, agricultural plant protection, photoelectric detection stability;vehicle navigation, vehicle satellite communications, forest and land monitoring, high-speed railway track inspection; hydrological Measurement, waterway detection, shipboard positioning communication, unmanned surface vehicle.

    Specifications

    Parameter Test condition Min value Typical value Max value Unit
    Gyroscope
    Measuring range ±450 º/s
    Bias stability 1s smoothing, rms 10 º/h
    Bias instability Allan variance 0.3 º/h
    Random Walk 0.15 º/√h
    Bias Repeatability 10 º/h
    Full temperature bias -40 ~ 80 °C, 10s smoothing 0.01 º/s
    Scale factor non-linearity FS=450 º/s 0.03 %FS
    Bandwidth(3dB) 250 Hz
    Accelerometer
    Measuring range     ±20   g
    Bias stability Allan variance   2 mg
    Random Walk 0.005 m/s/√h
    Bias Repeatability 1 σ 5 mg
    Full temperature bias -40 ~ 80 °C, 10s smoothing 5 mg
    Scale factor non-linearity FS=8g 0.1 %FS
    Bandwidth 250 Hz
    Magnetometer
    Dynamic measurement range ±2.5 Gauss
    Resolution 120 uGauss
    Noise Density 50 uGauss
    Bandwidth 200 Hz
    Barometer
    Pressure range 450 1100 mbar
    Overall error 6
    Resolution 0.1 mbar
    Absolute measurement accuracy 1.5 mbar
    Long-term stability ±1 mbar/yr
    Communication Interface
    1 way SPI Baud rate 15 MHz
    Electrical specification
    Voltage 2.5 3.3 12 V
    Power dissipation 1.5 W
    Ripple wave P-P 100 mV
    Structural characteristics
    Dimension 47×44×14mm
    Weight 50 g
    Operating environment
    Operating temperature -40 80
    Storage temperature -45 85
    Vibration 6.06g,10~2000Hzs
    Impact 2000g,0.1ms

    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