IMU/VRU/AHRS

ER-MIMU-10 (6 deg/hr)
1. Stable heading output;
2. 3 ° dynamic attitude accuracy;
3. Industrial-grade inertial sensors.

IMU/VRU/AHRS

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    Introduction

    ER-MIMU-10  IMU/VRU/AHRS

    Introduction
    The ER-MIMU-10 inertial sensing system integrates industrial-grade MEMS gyroscope and accelerometer, which can output 3D angular velocity, acceleration, magnetic field information, and fused 3D azimuth angles.When connected to a satellite navigation (GNSS) signal, fused position and velocity information can be output. ER-MIMU-10 includes ER-MIMU-10U Inertial Measurement Unit (IMU), ER-MIMU-10V Vertical Reference System (VRU), ER-MIMU-10A Attitude Reference System (AHRS)

    The ER-MIMU-10 is embedded with  multi-sensor fusion algorithm, which has been calibrated at the factory in all temperature ranges to ensure the excellent performance of the system in harsh environments. The compact design of the ER-MIMU-10 makes it easy for customers to integrate applications and shorten the development cycle.

    The ER-MIMU-10 has a dynamic attitude detection accuracy of 0.3° and provides a stable, low-drift relative heading output and a drift-free absolute heading output. It can meet the attitude, direction stability control, positioning and navigation needs of various carriers in complex and harsh application environments.

    Application
    Robots, unmanned vehicles
    Construction machinery, intelligent agricultural machinery
    Satcom on the move/Communication in Moving

    Product model information

                                                                        ER-MIMU-10U                   ER-MIMU-10V                      ER-MIMU-10A
    Angular velocity, acceleration                                   √                                       √                                         √
    Attitude angle                                                                                                    √                                         √
    Relative heading angle                                                                                     √                                          √
    Absolute heading angle                                                                                                                                √

    Specifications:

    Attitude orientation performance

    Attitude angle0.3 °1σ RMS
    Heading angleRelative heading angle*

    Absolute heading angle**

    0.8 °1σ RMS
    1 °1σ RMS
    Sensor parameters
    GyroscopeAccelerometerMagnetic sensors
    Range                                    ±500 °/s±16g±8 Gauss
    Non-linearity                          ±0.05%FS±0.5%FS±0.2%FS
    Bias instability***                    6 °/h0.05mg-
    Noise density                         0.015 °/s/√ Hz100μg/√ Hz0.4mG (RMS)
    Bandwidth                              116Hz116Hz-
    System parameters
    Input voltage                                3.3- 16VDCSize37.7*24*9.5mm
    Power consumption                     250mWWeight15.5g
    Operating temperature                 -40~85℃Hardware interfaceSPI UART
    Output frequency200Hz
    Note: The above parameters are typical values

    * Provides a relative heading angle without reference,Regular motion drift<0.8 °/min,Static drift<0.8 °/hr。

    ** In a homogeneous magnetic field environment

    *** Allan variance,1σ @25℃


    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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