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Low Cost Mems Inertial Measurement Unit For Attitude Control

Low-cost MEMS IMU for Attitude Control

ER-MIMU-184
1.Gyroscopic bias instability: 1 deg/hr.
2. -40~80°C temperature compensation.
3.Low cost.

Low-cost MEMS IMU for Attitude Control

Low Cost Mems Inertial Measurement Unit For Attitude Control

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    Introduction

    Low-cost MEMS IMU for Attitude Control

    Introduction
    ER-IMU-184 is a high-reliability and high-precision six-axis small-sized inertial measurement unit. The inertial sensing system integrates navigation-grade MEMS three-axis gyroscope and three-axis accelerometer. The angular rates and accelerations outputted are filtered and calibrated excellently, enabling ER-IMU-184 to provide precise inertial data under harsh conditions.

    ER-IMU-184 offers multiple configurable industrial standard communication interfaces and a wide input voltage range, facilitating its integration into various systems. It also features a small size, low power consumption, and high precision. It is an ideal choice for attitude measurement and navigation in most marine unmanned aerial vehicle on-board applications.

    Feature
    Size:65*51*35.5
    Weight:140
    -40~80°C temperature compensation
    The product is low-cost
    Gyro bias instability: 1deg/hr
    Gyro bias stability (10s 1σ): 4deg/hr
    Gyro angular random walk: 0.2 °/√h
    Accelerometer bias repeatability: 100ug
    Accelerometer bias stability (10s) (1σ): <50ug
    Accelerometer class II non-linearity coefficient: <100ug/g²

     Application
    Robotic control & orientation in autonomous machines, unmanned vehicles
    Azimuth, attitude, position measuring and keeping in GNSS-assisted INS
    Pitch, roll measuring in AHRS for UAV
    Motion survey and keeping in MRU
    Attitude & azimuth keeping, positioning in IMU
    Guidance, navigation, control in tactical MEMS system
    Stabilizing & Pointing in satellite antenna, target tracking system

    Specification

    Item Parameter Unit
    Gyro performance A B /
    Range 400 400 deg/s
    Scale Factor at 25°C 20000 20000 LSB/deg/s
    Scale Factor VS Temperature (1σ) 500 500 ppm
    Scale Factor Non-Linearity (1σ) <200 200 ppm
    Bias Instability (1σ 25℃) 3 1 deg/hr
    Bias Stability (10s 1σ) 5 4 deg/hr
    Angular Random Walk <0.25 <0.2 °/ √h
    Bias Repeatability (1σ 25℃) 5 4 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 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 (power supply 6V) 2 W
    Communication interface RS-422  
    Physical characteristics
    Size 65*51*35.5 mm
    Weight 140 g

    Dimension

    001 Dimension Of 18 Series Inertial Products


    Application Techniques

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