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North Seeking Mems Inertial Measurement Unit

2-Axis North-Seeking MEMS Gyro

ER-2MG-181
1.Gyro bias instability: < 0.01 deg/hr;
2.Gyro bias stability (10s, 1σ): < 0.05 deg/hr;
3.Gyro angle random walk: < 0.0025 °/√h.

2-Axis North-Seeking MEMS Gyro

North Seeking Mems Inertial Measurement Unit

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    Introduction

    2-Axis North-Seeking MEMS Gyro

    Introduction
    The ER-2MG-181 two-axis north-seeking MEMS gyroscope is small in size, light in weight, and has a simple structure with 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-181 Unit
    A B C
    Range 50 100 200 deg/s
    Bandwidth (-3dB) 12 12 50 Hz
    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
    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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