Product North Seeker Banner1
High Reliability Fog imu

 High Accuracy FOG IMU

ER-FIMU-40:
1.No wearing parts, long service life and high reliability
2. Small in size, light in weight, and easy to integrate
3. Fast dynamic response, suitable for complex motion scenarios

 High Accuracy FOG IMU

High Reliability Fog imu

Get Price Now



    Share to:

    Introduction

    ER-FIMU-40 High Accuracy FOG IMU

    ER-FIMU-40 FOG inertial measurement unit is specially developed for tactical system applications. The product consists of all solid-state three-axis fiber optic gyroscope, three-axis quartz flexible accelerometer, body structure, data interface board and other components.

    Features

    • It does not rely on external signals such as GPS/BDS and base stations. It can work independently in underground, underwaterand GPS-denied environments, providing continuous angular velocity and linear velocity data.
    • No wearing parts, long service life and high reliability
    • Fast dynamic response, suitable for complex motion scenarios
    • Wide temperature range operation: -50℃ to +80℃. Suitable for extreme temperature and humidity scenarios such as polar regions, upper air, and deserts, without performance degradation
    • Small in size, light in weight, and easy to integrate

    Applications

    • Communication satellite antenna pointing
    • Underwater robots (ROV/AUV), underwater cleaning equipment
    • The primary/backup inertial navigation systems for helicopters (rescue, mapping, transportation types), suitable for low-altitude flights and mountain rescue scenarios
    • Coal seam mining, underground mining equipment for non-ferrous metal mines
    • Geographic information mapping, such as urban topographic mapping and farmland water conservancy mapping
    • Subway tunnel boring machine (TBM)
    • Medium and large-sized civilian unmanned aircraft

    Specifications

    Gyroscope:

    No. Item Unit Parameter
    1 Measuring range º/s -500~+500
    2 Bias stability (1σ 10s) º/h ≤0.1
    3 Bias stability(1σ 100s) º/h ≤0.035
    4 Bias repeatability º/h ≤0.1
    5 Random walk coefficient º/√h ≤ 0.01
    6 Scale factor non-linearity ppm ≤50
    7 Scale factor repeatability ppm ≤ 50
    8 Scale factor asymmetry ppm ≤ 50
    9 Bandwidth Hz ≥500

    Accelerometer:

    No. Item Unit Parameter
    1 Range g ±50
    2 Threshold/Resolution μg 5
    3 Bias mg ≤ (±5)
    4 0g 4 Hours short time stability μg ≤30
    5 1g 4Hours short time stability μg ≤30
    6 Bias repeatability μg ≤40
    7 Scale factor mA/g 1.3±0.2
    8 Class II non-linearity μg /g2 ≤ (±30)
    9 Scale factor repeatability ppm ≤50
    10 Class II non-linearity repeatability μg /g2 ≤ (±30)
    11 Noise (840ΩSampling resistor) mv ≤8.4
    12 Bandwidth Hz 800~2500Hz

    IMU:

    No. Item Unit Parameter
    1 Dimensions mm 100×100×75
    2 Operating temperature -50~+80
    3 Data output rate Hz 200
    4 Data update rate Hz 1~1000 (Adjustable)
    5 Weight Kg 1.0±0.06
    6 Power supply V 28
    7 Communication interface / RS-422  (Customizable)

    Data update frequency: Adjustable from 1 to 1000Hz

    Byte Data Content Supplementary explanation
    1~4 Head 0X EB8055AA
    5~8 X Gyro data Low first, then high, dimensionless numerical quantity
    9~12 Y Gyro data Low first, then high, dimensionless numerical quantity
    13~16 Z Gyro data Low first, then high, dimensionless numerical quantity
    17~20 X Accl data Low first, then high, dimensionless numerical quantity
    21~24 Y Accl data Low first, then high, dimensionless numerical quantity
    25~28 Z Accl data Low first, then high, dimensionless numerical quantity
    29~30 Temperature Low first, then high
    31~33 End 0X 00FF34

    The connector wiring definitions are shown in the table below:

    No J30 Define Note
    1 1、3 12~28V Power
    2 2、4 GND
    8 8 T+ 422
    9 9 T-
    10 11 R-
    11 10 R+

     


    Application Techniques

    1.Internal Structure Analysis of IMU

    2.What are the Application Scenarios of the IMU?

    3.Application of IMU in UAV Flight Control System

    4.IMU in Drones (MEMS triaxial accelerometer, triaxial gyroscope, triaxial magnetometer)

    5.What is an IMU?

    6.IMU inertial measurement unit (provides odometer, position, attitude)


    More Products

    Low Cost 3 Axis FOG North Seeker
    Low Cost 3 Axis FOG North Seeker
    Low Cost FOG Gyroscope
    High Precision FOG North Seeker
    Small Size FOG Gyroscope
    Small Size FOG Gyroscope
    High Performance Quartz Accelerometer
    High Performance Quartz Accelerometer
    Low Cost FOG INS
    Low Cost FOG INS
    FOG IMU
    ER-FIMU-70 FOG IMU
    Ask for a Quote



      Menu