High Precision Navigation Mems Imu

High Accuracy North-Seeking MEMS IMU

ER-MIMU-05
1. Smallest Size: 38.6mm x 44.8mm x25.5mm;
2. Range can be selected;
3. Light weight: ≤70g.

High Accuracy North-Seeking MEMS IMU

High Precision Navigation Mems Imu

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    Introduction

    Parameters of High Accuracy North-Seeking MEMS IMUApplication of High Accuracy North-Seeking MEMS IMUIntroduction of High Accuracy North-Seeking MEMS IMU

    ER-MIMU-05 High Accuracy North-Seeking MEMS IMU

    Introduction
    ER-MIMU-05 is the world’s smallest six axis MEMS IMU. Inertial Measurement Unit, referred to as IMU, is a device to measure the attitude angle (or angular velocity) and acceleration of the three axis of the object. With the built-in accelerometer sensor and gyroscope, the IMU can measure the linear acceleration and rotation angular velocity from three directions and can obtain the attitude, velocity and displacement information of the carrier through the resolving.

    Features
    Smallest Size: 38.6mm x 44.8mm x25.5mm
    Range can be selected
    Light weight: ≤70g
    Temperature compensation: -40℃~ + 80℃
    Products with wide voltage design: 6v~12v
    Gyro bias instability up to: <0.01 deg/hr
    Gyro bias stability up to (10s 1σ): <0.05 deg/hr
    Gyro angular random walk up to: <0.0025 °/√h
    Accelerometer bias repeatability: 100ug
    Accelerometer bias stability (10s 1σ): <50ug
    Accelerometer class II non-linearity coefficient: <100ug/g2
    6V power supply, low power consumption 2W
    RS422 bus communication, baud rate from 230400~921600 can be set

    Application
    Initial alignment in UAV launch systems
    Guidance and navigation in navigation grade MEMS system
    Orientating and positioning in railway train system
    Precision platform attitude measuring and controls
    Precision attitude, position measuring in navigation grade MEMS IMU/INS
    North finding and positioning in land surveying/land mobile mapping system
    Bridge, tall building, tower, dam monitoring
    Rock and soil monitoring

    Specifications 

    Item Parameter Unit
    Gyro performance A B C /
    Range 50 100 200 deg/s
    Scale Factor at 25°C 160000 80000 40000 LSB/deg/s
    Scale Factor Repeatability (1σ) <50 <50 <100 ppm
    Scale Factor VS Temperature (1σ) ±300 ±300 ±300 ppm
    Scale Factor Non-Linearity (1σ) <200 <200 <300 ppm
    Bias Instability (1σ 25℃) <0.01 <0.02 <0.02 deg/hr
    Bias stability (10s 1σ) <0.05 <0.1 <0.1 deg/hr
    Angular Random Walk <0.0025 <0.005 <0.005 °/√h
    Bias Repeatability (1σ 25℃) <0.1 <0.1 <0.1 deg/hr
    Accelerometer performance
    Range 30 g
    Bias Stability (10s 1σ) <50 ug
    Bias Month Repeatability(1σ) 100 ug
    Bias Temp Coefficient <20 ug/℃
    Bias Temp Hysteresis <1.5 mg
    Scale Factor Non-linearity <500 ppm
    Scale Factor Month Repeatability <30 ppm
    Scale Factor Temp Coefficient 10 ppm/℃
    Class II Non-linearity Coefficient <100 ug/g2
    Scale Factor 250000 Lsb/g
    Environment and power
    Operate temperature -40~+80
    Storage temperature -55~+105
    Power supply 6~12V V
    Power 2 W
    Communication interface RS-422
    Physical characteristics
    Size 38.6 x 44.8 x 25.5 mm
    Weight ≤70 g

    Dimension


    Application Techniques

    1.How is IMU used?

    2.What is the Difference Between IMU and AHRS?

    3.SHow Does an IMU Work?

    4.Application of IMU in the Field of Drones

    5.Choosing an IMU: FOG IMUs vs MEMS IMUs

    6.IMU working principle & Tactical grade IMU product recommendations


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