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ER-AMM-2 Attitude Measurement Module

ER-AMM-2:
Attitude measurement type module
MEMS gyros and MEMS accelerometer
Low-cost and high reliability
Low power consumption
OEM modular design, several shapes optional

ER-AMM-2 Attitude Measurement Module

High Precision Stable Control Mems Imu.jpg

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    Introduction

    Introduction

    ER-AMM-2 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 ER-AMM-2 attitude measurement module. With the built-in accelerometer sensor and gyroscope, ER-AMM-2 can measure the linear acceleration and rotation angular velocity from three directions and can obtain the attitude, velocity.

    ER-AMM-2 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 data without the 15-pin plug provided by our company.

    Features

    Attitude measurement type module

    MEMS gyros and MEMS accelerometer

    Low-cost and high reliability

    Low power consumption

    OEM modular design, several shapes optional

    Application

    Robotic control & orientation in autonomous machines, unmanned vehicles

    Azimuth, attitude, position measuring and keeping in GNSS-assisted INS

    Pitch, roll measuring in AHRS for UAV

    Motion survey and keeping in MRU

    Stabilizing & pointing in satellite antenna

    Specifications

    Parameters ER-AMM-201 ER-AMM-202 Unit
    Gyro      
    Input Range 400 400 dps
    Scale factor 16000 20000 LSB/°/s
    Scale factor non-linearity <50 200 ppm
    Scale factor temp drift (1σ) 300 500 ppm
    Scale factor repeatability (1σ) <300 <10 ppm
    Bias temp drift (1б) 50 50 dph
    Bias temp drift (1б) (After temp compensation) <10 20 dph
    Bias stability (1б 10s) <3 5 dph
    Bias stability (1б 1s) <9 15 dph
    Bias Repeatability <3 5 dph
    Accelerometer      
    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 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
    Size A :70*65*45mm

    ER-AMM-2 Attitude Measurement Module

    B: 38.6 x 44.8 x 25.5mm

    ER-AMM-2 Attitude Measurement Module

    C:47×44×14mm:

    ER-AMM-2 Attitude Measurement Module

     
    Weight A : ≤220g(withshell)

    ≤100g(without shell and baseboard)

    B: ≤70g

    C:≤40g


    Application Techniques

    1.Do you know the core components that give precise control to automated equipment

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    6.From flight control to fault diagnosis, how does IMU dominate drones?


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