Low Power Inertial Measurement Unit

Low Power Inertial Measurement Unit

ER-MIMU-10
1. Mini Diameter: 120mm x Φ30mm;
2. Light weight: ≤150g;
3. Temperature compensation: -40℃~ + 80℃.

Low Power Inertial Measurement Unit

Low Power Inertial Measurement Unit

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    Introduction

    Low Power Inertial Measurement Unit

    Introduction
    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 rapid development of science and technology, MEMS IMU is increasingly widely used in the fields of oil and mining, injecting new vitality into this traditional industry. This is a high-performance product specially designed for oil drilling, mining and other fields. Based on three-axis integrated MEMS gyro and three-axis accelerometer, ER-MIMU-10 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
    Mini diameter: 120mm x Φ30mm
    Light weight: ≤150g
    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
    Antenna and 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 A B Unit
    Gyro performance
    Range 300 400 deg/s
    Scale Factor at 25°C 28000 20000 LSB/deg/s
    Scale Factor Repeatability (1σ) <50 <20 ppm
    Scale Factor VS Temperature (1σ) ±300 ±100 ppm
    Scale Factor Non-Linearity (1σ) <300 <100 ppm
    Bias Instability(1σ 25℃) 0.03 0.05 deg/hr
    Bias stability (10s 1σ) <0.15 <0.5 deg/hr
    Angular Random Walk <0.01 <0.025 °/ √h
    Bias Repeatability(1σ 25℃) <0.3 <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 120 x Φ30 mm
    Weight ≤150 g

    Dimension

    Figure 1 Product Outline(unit:mm)

    Figure 2 Product Polarity Diagram


    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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