Er Mimu 02

High Performance Navigation MEMS IMU

ER-MIMU-02 (0.05 deg/hr)
1. 3 axis gyroscope & 3-axis accelerometer;
2. Gyro bias instability: 0.05 deg/hr;
3. Gyro angular random walk:<0.025°/ √h;
4. Gyro bias stability (10s 1σ): <0.5deg/hr.

High Performance Navigation MEMS IMU

Er Mimu 02

Get Price Now



    Share to:

    Introduction

    Application of High Performance Navigation MEMS IMUIntroduction of High Performance Navigation MEMS IMUHigh-Performance-Navigation-MEMS-IMU for Antenna

    ER-MIMU-02 High Performance Navigation MEMS IMU

    Introduction
    Inertial Measurement Unit, referred to as IMU, is a device to measure the attitude angle (or angular velocity) and acceleration of the three axis of the object. Gyroscope and accelerometer are the core devices of inertial navigation system (INS). With the built-in accelerometer sensor and gyroscope, the IMU can measure the linear acceleration and rotation angular velocity from three directions and can obtain the attitude, velocity and displacement information of the carrier through the resolving.
    ER-MIMU-02 uses MEMS accelerometer and gyroscope with high quality and reliability, RS422 and external communication, baud rate can be flexibly set between 230400~921600, through the communication protocol to set the user's required communication baud rate. With X, Y, Z three-axis precision gyro, X, Y, Z three-axis accelerometer with high resolution, can be output by RS422 X, Y, Z three axis of gyroscope and accelerometer's original hexadecimal complement data (including gyro hexadecimal complement the numerical temperature, angle, the accelerometer hexadecimal temperature, the acceleration hexadecimal complement number); It can also output float dimensionless values of the gyroscope and accelerometer processed by the underlying calculation.

    Features
    Gyro bias instability:0.05deg/hr
    Gyro bias stability (10s 1σ): <0.5deg/hr
    Gyro angular random walk:<0.025 °/√h
    Weight:≤100g (without shell)
    ≤220g (with shell)
    Operate Temp:-40℃~ + 80℃
    Accelerometer bias repeatability: 200-500ug
    Accelerometer bias stability (1s) (1σ): <30ug
    Accelerometer class II non-linearity coefficient: <100ug/g2
    Baud rate can be flexibly set between 230400~921600
    High-performance navigation

    Application 
    Antenna and Line of Sight Stabilization Systems
    Integrated Navigation Systems & Inertial Guidance System
    Flight Control & Guidance System
    Attitude Heading Reference Systems (AHRS)
    Stabilization of Antennas, Cameras & Platforms
    Aerial and Marine Geo-mapping / Surveying

    Specifications

    Item Parameter Unit
    Gyro performance
    Range 400 deg/s
    Bandwidth (-3dB) 100 Hz
    Scale Factor at 25°C 20000 LSB/deg/s
    Scale Factor Repeatability (1σ) <20 ppm
    Scale Factor VS Temperature (1σ) 100 ppm
    Scale Factor Non-Linearity (1σ) 100 ppm
    Bias Instability 0.05 deg/hr
    Bias stability (10s 1σ) <0.5 deg/hr
    Angular Random Walk <0.025 °/ √h
    Bias error over temperature (1σ) 3 deg/hr
    Bias temperature variations, calibrated (1σ) <0.5 deg/hr
    Bias Run-Run (1σ) <0.3 deg/hr
    Accelerometer performance
    Range 30 g
    Bandwidth 100 Hz
    Bias Stability (1s) (1σ) <30 ug
    Bias Repeatability 200-500 ug
    Bias Temp Coefficient <20 ug/℃
    Bias Temp Hysteresis <0.5 mg
    Factor Scale Non-linearity <500 ppm
    Factor Scale Repeatability <300 ppm
    Factor Scale Temp Coefficient 10 ppm/℃
    Class II Non-linearity Coefficient <100 ug/g2
    Factor Scale 400000-800000 μg/LSB
    System Performance
    Supply Voltage 6~12V
    Supply Consumption 2W
    Interface RS422
    Vibration 6.06g (10~2000Hz)
    Shock 5000g, 0.1ms
    Operate Temp -40℃~ + 80℃
    Storage Temp -55℃~ + 105℃
    Weight ≤100g (without shell)

    ≤220g (with shell)

    Size 43.2mm*43.2mm*35.5mm (without shell)

    65mm*70mm*45.5mm (with shell)


    Application Techniques

    1.IMU working principle & Tactical grade IMU product recommendations

    2.How Does an IMU Work?

    3.Choosing an IMU: FOG IMUs vs MEMS IMUs

    4.Application of IMU in the Field of Drones

    5.What is the Difference Between IMU and AHRS?

    6.How is IMU used?


    More Products

    North Seeking Mems Imu For Gyro Tools
    North-Seeking MEMS IMU for Gyro Tools

    High Performance Navigation MEMS IMU
    High Performance Navigation MEMS IMU
    High Performance Mems Imu
    High Performance MEMS IMU

    High Precision Navigation MEMS IMU
    High Precision Navigation MEMS IMU
    North Seeking Mems Imu For Gyro Tools
    Low Power Inertial Measurement Unit

    High Precision Stable-Control MEMS IMU
    Aerospace, Oil and Gas, Mining, Mapping
    Ask for a Quote



      Menu