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High Performance Navigation Mems Inertial Measurement Unit

High-performance Navigation 2 axis MEMS Gyro

ER-2MG-182
1.Gyro bias instability: 0.03 deg/hr;
2.Gyro bias stability (10s 1σ): <0.15deg/hr;
3.Gyro angle random walk: <0.025 °/√h.

High-performance Navigation 2 axis MEMS Gyro

High Performance Navigation Mems Inertial Measurement Unit

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    Introduction

    High-performance Navigation 2 axis MEMS Gyro

    Introduction
    The ER-2MG-182 two-axis navigation MEMS gyroscope is small in size, light in weight, simple in structure and has good reliability. The dual-axis gyroscope has the greatest function of providing the angular velocity needed to determine the motion state of an object, and thus is also called a motion sensor.

    Application
    Construction machinery dip angle measurement, angle control, pylon operation monitoring, medical equipment angle control, satellite antenna star search, bridge, tall building, tower, dam monitoring and rock and soil monitoring, mining, attitude/heading reference system, integrated inertial navigation.

    Specification

    Parameter ER-2MG-182 Unit
    A B
    Range 300 400 deg/s
    Bandwidth (-3dB) 50 100 Hz
    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 0.03 0.03 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 <0.15 deg/hr
    Size 65*51*35.5 mm
    Weight 140 g
    Operate temperature -45~+85
    Storage temperature -55~+105

    Application Techniques

    1.Error Generation Mechanism of MEMS Gyroscope Under High Acceleration Condition

    2.Bandwidth test method of MEMS gyroscope

    3.Packaging of MEMS gyroscope: Structural Analysis of Deep Hole Packaging

    4.Research on scale factor nonlinearity of MEMS gyroscope

    5.Analysis of drive loop noise of MEMS gyroscope

    6.Bias Temperature Compensation Analysis of MEMS Gyroscope


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