Product North Seeker Banner1
High Accuracy North Seeking Mems Imu

High Precision Navigation MEMS IMU

ER-MIMU-06
1. Smallest volume: 38.6mm x 44.8mm x25.5mm;
2. Light weight: ≤70g;
3. Temperature compensation: -40℃~ + 80℃.

High Precision Navigation MEMS IMU

High Accuracy North Seeking Mems Imu

Get Price Now



    Share to:

    Introduction

    ER-MIMU-06 High Precision Navigation MEMS IMU

    Introduction
    ER-MIMU-06 is the world’s smallest six axis MEMS IMU. 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. 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.

    Features
    Smallest volume: 38.6mm x 44.8mm x25.5mm
    Light weight: ≤70g
    Temperature compensation: -40℃~ + 80℃
    Products with wide voltage design: 6v~12v
    Gyro bias instability: 0.03deg/hr
    Gyro bias stability (10s 1σ): <0.15deg/hr
    Gyro angular random walk: <0.01 °/√h
    Accelerometer bias repeatability: 100ug
    Accelerometer bias stability (10s 1σ): <50ug
    Accelerometer class II non-linearity coefficient: <100ug/g2
    6V power supply, low power consumption 2W
    RS422 bus communication, baud rate from 230400~921600 can be set

    Application
    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 A B Unit
    Gyro performance
    Range 300 400 deg/s
    Scale Factor at 25°C 28000 20000 LSB/deg/s
    Scale Factor Repeatability (1σ) <50 <20 ppm
    Scale Factor VS Temperature (1σ) 300 100 ppm
    Scale Factor Non-Linearity (1σ) <300 <100 ppm
    Bias Instability(1σ 25℃) 0.03 0.03 deg/hr
    Bias stability (10s 1σ) <0.15 <0.5 deg/hr
    Angular Random Walk <0.01 <0.025 °/ √h
    Bias Repeatability(1σ 25℃) <0.3 <0.15 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 DC V
    Power (Power supply 6) 2 W
    Communication interface RS-422
    Physical characteristics
    Size 38.6 x 44.8 x 25.5 mm
    Weight ≤70 g

    Dimension


    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?


    More Products

    North-Seeking MEMS IMUNorth-Seeking MEMS IMU
    High Accuracy North Seeking Mems ImuHigh Accuracy North-Seeking MEMS IMU
    North Seeking Mems Imu For Gyro Tools North Seeking Mems Imu For Gyro Tools
    High Performance North Seeking Mems Imu North-seeking MEMS IMU
    High Performance MEMS IMU
    High Performance MEMS IMU
    Economical MEMS GyroscopeEconomical MEMS Gyroscope
    Aerospace, Maritime, Mapping
    Ask for a Quote



      Menu