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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.Gyroscopic bias stability (10s 1σ): 5 deg/hr
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
    Low cost
    Gyroscopic bias instability: 1 deg/hr
    Gyroscopic bias stability (10s 1σ): 5 deg/hr
    Gyroscopic angle random walk: 0.25 °/√h

     Application
    Autonomous machine control and positioning in autonomous robots and unmanned vehicles
    Azimuth, attitude and position measurement and stabilization in GNSS-assisted INS
    Pitch and roll measurement in UAV AHRS
    Motion measurement and stabilization in MRU
    Attitude and azimuth stabilization, and positioning in IMU

    Specification

    Project Parameter Unit
    Gyroscope A B  
    Range 400 400 deg/s
    Scale factor(25°C) 20000 20000 LSB/deg/s
    Scale factor temperature drift (1σ) ±500 ±500 ppm
    Scale factor non-linearity (1σ) <200 200 ppm
    Bias instability (1σ at 25°C) 3 1 deg/hr
    Bias stability (10s at 1σ) 5 4 deg/hr
    Angle random walk <0.25 <0.2 °/√h
    Bias repeatability (1σ at 25°C) 5 4 deg/hr
    Accelerometer
    Range ±10,±20, ±40 g
    Cross-coupling sensitivity 1 %
    Scale factor ±10, ±20, ±40 19.5, 39, 78 ug/LSB
    Sensitivity temperature coefficient ±0.01 %/°C
    Repetition X, Y axis, Z axis 0.1, 0.2 %
    Non-linearity ±10g, ±40g 0.1, 1.3 % FSR
    Spectral density ±10, ±40 75, 90 ug/√Hz
    Random walk of velocity X, Y axis Z axis 38.2, 26.5 mm/sec/√Hr
    Low-pass filter bandwidth 0.977-1000 Hz

    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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