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High Performance Navigation Mems Inertial Measurement Unit

High-performance Navigation MEMS IMU

ER-MIMU-182
1.Gyroscope bias instability: 0.03 deg/hr
2.Gyroscope bias stability (10s 1σ): <0.5 deg/hr
3.High cost performance.

High-performance Navigation MEMS IMU

High Performance Navigation Mems Inertial Measurement Unit

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    Introduction

    High-performance Navigation MEMS IMU

    Introduction
    The Inertial Measurement Unit (IMU) is a device that measures the three-axis attitude angles (or angular velocities) and accelerations of an object. Gyroscopes and accelerometers are the core components of an Inertial Navigation System (INS). By using the built-in accelerometers and gyroscopes, the IMU can measure the three-axis linear accelerations and three-axis rotational angular velocities, and obtain the information of the carrier's attitude, velocity and displacement through analysis. The ER-MIMU-182 uses high-quality and highly reliable MEMS accelerometers and gyroscopes.

    Feature
    Gyroscope bias instability: 0.03 deg/hr
    Gyroscope bias stability (10s 1σ): <0.5 deg/hr
    Gyroscope angle random walk: <0.025 °/√h
    Accelerometer bias repeatability: 100 ug
    Accelerometer second-order nonlinearity: <100 ug/g²
    High-performance navigation

    Application
    Integrated navigation system and inertial guidance system
    Flight control system
    Attitude and heading reference system (AHRS)
    Stability of antennas, cameras and platforms
    Aeronautical and marine geographic surveying / mapping

    Specification

    Project Parameter Unit
    Gyroscope A B /
    Range 300 400 deg/s
    Scale factor(25°C) 28000 20000 LSB/deg/s
    Scale factor repeatability of (1σ) <50 <20 ppm
    Scale factor temperature drift (1σ) ±300 ±100 ppm
    Scale factor non-linearity (1σ) <300 <100 ppm
    Bias instability (1σ at 25°C) 0.03 0.03 deg/hr
    Bias stability (10s at 1σ) <0.15 <0.5 deg/hr
    Angle random walk <0.01 <0.025 °/√h
    Bias repeatability (1σ at 25°C) <0.3 <0.15 deg/hr
    Accelerometer
    Range 30 g
    Bias stability (10s 1σ) <50 ug
    Bias monthly repeatability (1σ) 100 ug
    Bias temperature coefficient <20 ug/℃
    Bias temperature hysteresis <1.5 mg
    Scale factor non-linearity <500 ppm
    Scale factor monthly repeatability <30 ppm
    Scale factor temperature coefficient 10 ppm/℃
    Scale factor ClassⅡnon-linearity coefficient <100 ug/g²
    Scale factor 250000 Lsb/g

    Application Techniques

    1.Do you know the core components that give precise control to automated equipment

    2.High-performance IMU: A New Benchmark for Precise Measurement and Control

    3.Industrial Versatile Tool: High Cost-Performance IMU Meets Diverse Needs

    4.Flight safety secrets: The core role of high-precision IMUs in aviation

    5.Revolutionizing drone navigation: How to redefine high performance and low cost

    6.From flight control to fault diagnosis, how does IMU dominate drones?


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