Low Power Consumption MEMS IMU

ER-MIMU-M01B(≤3°/h)
1. Miniaturized IMU
2. Low power consumption
3. High cost performance
4. Total temperature compensation

Low Power Consumption MEMS IMU

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    Introduction

    Introduction
    The M01B Low Power Consumption MEMS IMU is a general-purpose, miniaturized component that contains three-axis gyroscope and three-axis accelerometer information. Temperature compensation is performed through the bias stability and scale of each axis to improve its measurement accuracy.

    Features
    Miniaturized IMU
    Low power consumption
    High cost performance
    Total temperature compensation

    Application 
    Inertial navigation: inertial guidance, integrated navigation, platform stability
    Short-term navigation: flight control, ballistic correction, telemetry and remote control
    Attitude control: UAV, antenna orientation

    Specifications

    Gyroscope
    Measuring range±450°/s
    Full temperature bias≤150°/h
    Angle random walk≤0.25°/ √h
    Bias instability≤3°/h
    Bias stability (1σ)≤12°/h
    Bias repeatability (1σ)≤12°/h
    Scale factor non-linearity≤50ppm
    Bandwidth (configurable)150Hz
    Accelerometer
    Measuring range±10g
    Full temperature bias≤5mg
    Rate random walk≤0.03m/s/√h
    Bias instability≤0.04mg
    Bias stability (1σ)≤0.3mg
    Bias repeatability (1σ)≤0.3mg
    Scale factor non-linearity (Within 1g)≤200ppm
    Bandwidth (configurable)150Hz
    System
    Supply voltage5V±0.3V
    Operating temperature range-45℃~+85℃
    Shock resistance≥2000g
    Vibration≥20grms
    Size22.4mm×22.4mm×9mm
    Weight≤30g
    Interface type(--)RS422
    Output mode(--)High temperature wire
    Output interface wiring definition
    Red conductorVCC(+5V)Power supply positive
    Black conductorGNDPower supply ground
    White conductorRx+RS422 receive +
    Brown conductorRx-RS422 receive -
    Green conductorTx-RS422 send -
    Yellow conductorTx+RS422 send +

     

    Dimensions


    Application Techniques

    1.IMU and GPS fusion algorithm principle

    2.MEMS IMU error analysis and compensation

    3.Reusable spacecraft IMU dynamic accuracy assessment method

    4.Research on MEMS IMU error modeling and temperature compensation technology

    5.Calibration method and error analysis of low-precision MEMS IMU

    6.MEMS-IMU error calibration compensation method that does not rely on precision turntable


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