Low Cost Attitude Control Mems Imu 

High Precision Stable Control MEMS IMU

ER-MIMU-03/03Mini
1. New mini version: 40*40*42mm(with shell)/27*26*34(without shell and baseboard);
2.  OEM modular design, strong applicability;
3. Gyro bias instability(1σ 25℃): <0.3deg/hr.

High Precision Stable Control MEMS IMU

Low Cost Attitude Control Mems Imu 

Get Price Now



    Share to:

    Introduction

    Introduction of High Precision NavigationStable Control MEMS IMUApplication areas of High Precision NavigationStable Control MEMS IMUHigh-Precision-NavigationStable-Control-MEMS-IMU for Heading

    ER-MIMU-03/03Mini High Precision Stable Control 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-03/03Mini uses MEMS accelerometer and gyroscope with high quality and reliability, RS422 and external communication.Default baud rate 921600 (customized). 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.

    A simple operation is required to connect our products to your system and obtain IMU data without the 15-pin plug provided by our company. At the same time, the size and weight of our products can be significantly reduced by removing the base plate housing.

    Features
    New mini version size: 40*40*42(mini version with shell)/27*26*34(mini version without shell and baseboard)
    Weight: 120g(mini version with shell)/ 80g(mini version without shell and baseboard)
    OEM modular design, strong applicability
    -40~80°C temperature compensation
    Gyro bias instability: <0.3deg/hr
    Gyro bias stability (10s 1σ): <3deg/hr
    Gyro angular random walk: <0.125 °/√h
    Accelerometer bias repeatability: 100ug
    Accelerometer bias stability (10s) (1σ): <50ug
    Accelerometer class II non-linearity coefficient: <100ug/g2
    Weight: ≤100g (without shell and baseboard)/≤220g (with shell)

    Application 
    Stabilization of Cameras & Platforms
    Azimuth, attitude, position measuring and keeping in GNSS-assisted INS
    Pitch, roll measuring in AHRS for UAV
    Motion survey and keeping in MRU
    Attitude & azimuth keeping, positioning in IMU
    Guidance, navigation, control in tactical MEMS system
    Stabilizing in satellite antenna, target tracking system
    Robotic Control & Orientation in autonomous machines, unmanned vehicles

    Specifications

    Item Parameter Unit
    Gyro performance
    Range 400 deg/s
    Scale Factor at 25°C 16000 LSB/deg/s
    Scale Factor Repeatability (1σ) <50 ppm
    Scale Factor VS Temperature (1σ) ±300 ppm
    Scale Factor Non-Linearity (1σ) <300 ppm
    Bias Instability (1σ 25℃) <0.3 deg/hr
    Bias stability (10s 1σ) <3 deg/hr
    Angular Random Walk <0.125 °/ √h
    Bias Repeatability (1σ 25℃) <3 deg/hr
    Accelerometer performance
    Range 30 g
    Bias Stability (10s 1σ) <50 ug
    Bias Repeatability 100 ug
    Bias Temp Coefficient <20 ug/℃
    Bias Temp Hysteresis <1.5 mg
    Scale Factor Non-linearity <500 ppm
    Scale Factor Month Repeatability <30 ppm
    Scale Factor Temp Coefficient 10 ppm/℃
    Class II Non-linearity Coefficient <100 ug/g2
    Scale Factor 250000 Lsb/g
    Environment and power
    Operate temperature -40~+80
    Storage temperature -55~+105
    Power supply 6~12V V
    Power (power supply 6V) 2 W
    Communication interface RS-422
    Physical characteristics
    Siz 70×65×45(with shell)/43.2×43.2×35.5 (without shell and baseboard)

    40*40*42(mini version with shell)/27*26*34(mini version without shell and baseboard)

    mm
    Weight ≤220(withshell)/≤100(without shell and baseboard)

    120g(mini version with shell)/ 80g(mini version without shell and baseboard)

    g

    Dimension

    Standard version

    Mini version

    Mini Version Of Cost Efficient Triaxial Mems North Seeker

    Dimension Of Mini Cost Efficient Triaxial Mems North Seeker


    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
    North-Seeking MEMS IMU
    North Seeking Mems Imu For Gyro Tools
    North-Seeking MEMS IMU for Gyro Tools
    High Precision Navigation Stable Control Mems ImuHigh Precision Stable Control MEMS IMU
    Er Mimu 10 Imu Vru Ahrs
    IMU/VRU/AHRS
    High Accuracy North-Seeking MEMS IMU
    Low Cost Mems Imu
    Low Cost MEMS IMU
    Land Vehicle, UAV
    Ask for a Quote



      Menu