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High Performance Mems Imu

High Performance MEMS IMU

ER-MIMU-M02
1.Dynamic  measurement range:±450º/s;
2. Bias instability: 2 º/h (Allan variance);
3.Angular random walk: 0.15º/√h.

High Performance MEMS IMU

High Performance Mems Imu

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    Introduction

    ER-MIMU-M02  High Performance MEMS IMU

    Introduction

    ER-MIMU-M02 is an inertial measurement unit (IMU) based on micromechanical technology (MEMS), including a built-in MEMS gyroscope with 2°/h (Allan)  bias instability and a MEMS accelerometer with 24μg (Allan) bias instability. It is used to measure the three-axis angular rate and three-axis acceleration of the carrier. Through the communication protocol, the gyroscope and accelerometer data with error compensation (including temperature compensation, installation misalignment Angle compensation, nonlinear compensation, etc.) can be solved to obtain the carrier attitude, velocity, displacement and other information. It also has a built-in three-axis magnetic sensor and air pressure sensor. The magnetometer helps with orientation and can be used to calibrate the data and orient it to the correct position. The product has high reliability and strong environmental adaptability.

    Features

    Three-axis digital gyroscope:

    Dynamic measurement range: ±450º/s;

    Bias instability: 2 º/h (Allan variance);

    Angular random walk: 0.15º/√h.

    Three-axis digital accelerometer:

    Dynamic measurement range: 16g;

    Bias instability: 24μg (Allan variance);

    High reliability: mean time between failures > 20000h;

    Ensure accuracy over the full temperature range (-40°C~80°C): Built-in high-performance temperature calibration and compensation algorithm;

    Communication interface: 1 SPI, slave mode.

    Application

    Space-based fields: unmanned aerial vehicles, aerial photography, agricultural plant protection, photoelectric detection stability;

    Land-based fields: vehicle navigation, vehicle satellite communications, forest and land monitoring, high-speed railway track inspection;

    Sea-based fields: hydrological Measurement, waterway detection, shipboard positioning communication, unmanned surface vehicle.

    Specifications

    Parameter Test condition Min value Typical value Max value Unit
    Gyroscope
    Measuring range ±450 º/s
    Bias instability Allan variance 2 º/h
    Bias stability 6 º/h
    Random Walk 0.15 º/√h
    Bias Repeatability 1 σ 6 º/h
    Bias temperature coefficient ±0.001 dps/℃
    Scale factor non-linearity 1 σ 0.01 %FS
    Bandwidth(3dB) 96 Hz
    Accelerometer
    Measuring range ±16 g
    Bias instability Allan variance 24 μg
    Bias stability 70 μg
    Bias Repeatability 1 σ 150 μg
    Bias temperature coefficient ±0.1 mg/℃
    Noise density 60 ug/√Hz
    Bandwidth(3dB) 83 Hz
    Magnetometer
    Dynamic measurement range ±2.5 Gauss
    Resolution 120 uGauss
    Noise Density 50 uGauss
    Bandwidth 200 Hz
    Barometer
    Pressure range 450 1100 mbar
    Overall error 6
    Resolution 0.1 mbar
    Absolute measurement accuracy 1.5 mbar
    Long-term stability ±1 mbar/yr
    Communication Interface
    1 way SPI Baud rate 15 MHz
    Electrical specification
    Voltage 3 3.3 3.6 V
    Power dissipation 1.5 W
    Ripple wave P-P 100 mV
    Structural characteristics
    Dimension 47×44×14mm
    Weight 50 g
    Operating environment
    Operating temperature -40 80
    Storage temperature -45 85
    Vibration 3g, 10~2000Hz
    Impact 30g, 11ms
    Mean time between failures 20000 h
    Reliability
    Continuous working hours 120 h

     

    Dimension

    Dimensions Of High Performance Mems Imu(16488)

    Coordinate system definition

    The coordinate systems for the 3 gyroscopes (x g, y g, z g) and 3 accelerometers (x a, y a, z a) are defined as shown in the figure below, with the arrows in a positive direction.

    Read and write data

    ER-MIMU-M02 is an autonomous sensor system that automatically activates when an active power supply is present. Once the initialization process is complete, it begins sampling, processing, and loading the calibrated sensor data into the output registers, which can be accessed via the SPI port. The SPI port is usually connected to a compatible port of the embedded processor, and the connection diagram is shown in the figure. Four SPI signals support synchronous serial data transmission. In the factory default configuration, the DIO2 pin provides a data-ready signal; When new data is available in the output data registers, the pin goes high.

    M01

    1 General Purpose Host Processor SPI Settings

    Processor settings introduce
    Host mode ER-MIMU-M02 used as a slave
    SCLK ≤ 15 MHz Maximum serial clock rate
    SPI mode 3 CPOL = 1 (polarity), CPHA = 1 (phase)
    MSB Priority mode Positional order
    16-bit mode Shift register/data length

    2 SPI Communication

    If the previous command is a read request, the SPI port supports full-duplex communication, and the external processor can write DIN at the same time as reading DOUT, as shown in the following figure.

    M02

    2.1 SPI read and write timing

    Read sensor data

    The ER-MIMU-M02 automatically starts and activates page 0 for data register access. After accessing any other page, the 0x00 should be written to the PAGE_ID register (DIN = 0x8000) to activate page 0 in preparation for subsequent data access. A single register read operation requires two 16-bit SPI cycles. In the first cycle, the bit allocation function in Figure 1 is used to request a read of the contents of a register; In the second cycle, the register contents are output via DOUT. The first digit of the DIN command is 0, followed by the high or low address of the register. The last 8 bits are extraneous, but the SPI requires the full 16 SCLKs to receive requests. The following diagram shows two consecutive register reads, first DIN = 0x1A00, requesting the contents of the Z_GYRO_OUT register, and then DIN = 0x1800, requesting the contents of the Z_GYRO_LOW

    M03

    2.2 Example of an SPI read operation

    User Register Memory Mapping

    R/W PAGE_ID address default Register description
    R/W 0x00 0x00 0x00 Page identifier
    R 0x00 0x0E N/A temperature
    R 0x00 0x10 N/A x axis gyroscope output, low word
    R 0x00 0x12 N/A x axis gyroscope output,high word
    R 0x00 0x14 N/A y axis gyroscope output, low word
    R 0x00 0x16 N/A y axis gyroscope output,high word
    R 0x00 0x18 N/A z axis gyroscope output, low word
    R 0x00 0x1A N/A z axis gyroscope output,high word
    R 0x00 0x1C N/A x axis accelerometer output, low word
    R 0x00 0x1E N/A x axis accelerometer output,high word
    R 0x00 0x20 N/A y axis accelerometer output, low word
    R 0x00 0x22 N/A y axis accelerometer output,high word
    R 0x00 0x24 N/A z axis accelerometer output, low word
    R 0x00 0x26 N/A z axis accelerometer output,high word
    R 0x00 0x28 N/A x axis Magnetic output,high word
    R 0x00 0x2A N/A y axis Magnetic output,high word
    R 0x00 0x2C N/A z axis Magnetic output,high word
    R 0x00 0x2E N/A Barometric pressure output,low word
    R 0x00 0x30 N/A Barometric pressure output,high word

    2.3 Transform formulas

    Current temperature =25+ TEMP_OUT* 0.00565

    X axis gyroscope for example X_GYRO_OUT X_GYRO_LOW
    1LSB=0.02°/S The weight of the MSB is 0.01°/s, and the weight of the successors is half that of the previous one
    0.02*X_GYRO_OUT 0.01*MSB+0.005*.......

    YZ gyroscopes are calculated in a similar way to X-axis gyroscopes。

    X axis accelerometer for example X_ACCL_OUT X_ACCL_LOW
    1LSB=0.8mg The weight of the MSB is 0.4mg, and the weight of the successors is half that of the previous one
    0.8*X_ACCL_OUT 0.4*MSB+0.2*.......

    YZ accelerometers are calculated in a similar way to X-axis accelerometers。

    X x axis Magnetic X_MAGN_OUT
    1LSB=0.1mGauss
    0.1*X_MAGN_OUT

    YZ axis magnetometers are calculated in a similar way to X-axis magnetometers。

    Example of barometric pressure calculation BAROM_OUT BAROM_LOW
    1LSB=40ubar The MSB is weighted at 20ubar, and the successors are weighted half the weight of the previous one
    40*BAROM_OUT 20*MSB+10*.......

    Note: For gyroscope, accelerometer, magnetic fraction high 16bit, and low 16bit, the final result of addition is calculated separately

    M04

    Electrical interfaces

    Pin serial number name type description
    10,11,12 VDD power supply
    13,14,15 GND Power Ground
    7 DIO1 I/O Generic I/O, configurable
    9 DIO2 I/O
    1 DIO3 I/O
    2 DIO4 I/O
    3 SPI-CLK input The SPI defaults to slave mode
    4 SPI-MISO output
    5 SPI-MOSI input
    6 SPI-CS input
    8 RST input reposition
    16~24 NC spare Manufacturer reserved

    Exterior structure

    M05

    The product is mounted through 4XΦ2.4 through holes, and 4XM2 screws (plus elastic washers and flat washers) are used for mounting. When the connector is installed, the plug should be connected to the receptacle. The product mating connector is Samtec CLM-112-02-L-D


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