High Accuracy North Seeking Mems Imu

High Precision Navigation MEMS IMU

ER-MIMU-06
1. Smallest Size: 38.6mm x 44.8mm x25.5mm;
2. Light weight: ≤70g;
3. Temperature compensation: -40℃~ + 80℃.

High Precision Navigation MEMS IMU

High Accuracy North Seeking Mems Imu

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    Introduction

    ER-MIMU-06 High Precision Navigation MEMS IMU

    Introduction
    ER-MIMU-06 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
    Light weight: ≤70g
    Temperature compensation: -40℃~ + 80℃
    Products with wide voltage design: 6v~12v
    Gyro bias instability: 0.05deg/hr
    Gyro bias stability (10s 1σ): <0.5deg/hr
    Gyro angular random walk: <0.025 °/√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
    Line of Sight Stabilization Systems
    Integrated Navigation Systems & Inertial Guidance System
    Flight Control & Guidance System
    Attitude Heading Reference Systems (AHRS)
    Stabilization of Antennas, Cameras & Platforms
    Aerial and Marine Geo-mapping / Surveying

    Specifications

    Item Parameter Unit
    Gyro performance
    Range 400 deg/s
    Scale Factor at 25°C 20000 LSB/deg/s
    Scale Factor Repeatability (1σ) <20 ppm
    Scale Factor VS Temperature (1σ) ±100 ppm
    Scale Factor Non-Linearity (1σ) <100 ppm
    Bias Instability (1σ 25℃) 0.05 deg/hr
    Bias stability (10s 1σ) <0.5 deg/hr
    Angular Random Walk <0.025 °/ √h
    Bias Repeatability (1σ 25℃) <0.3 deg/hr
    Accelerometer performance
    Range 30 g
    Bias Stability (10s 1σ) <50 ug
    Bias Repeatability 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 DC V
    Power (Power supply 6) 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.Introduction of High-precision Navigation MEMS IMU–ER-MIMU-02 and ER-MIMU-06

    2.What are the advantages of MEMS IMU?

    3.Internal Structure Analysis of IMU

    4.What are the Application Scenarios of the IMU?

    5.Software Debugging of MEMS IMU ER-MIMU-01!

    6.Application of IMU in UAV Flight Control System


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