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Inertial Measurement Unit High Precision MEMS Inertial Navigation Vehicle Navigation Voltage 3.0~3.6V,One SPI 15MHz

Xi'an Kacise Optronics Co.,Ltd.
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    Buy cheap Inertial Measurement Unit High Precision MEMS Inertial Navigation Vehicle Navigation Voltage 3.0~3.6V,One SPI 15MHz from wholesalers
     
    Buy cheap Inertial Measurement Unit High Precision MEMS Inertial Navigation Vehicle Navigation Voltage 3.0~3.6V,One SPI 15MHz from wholesalers
    • Buy cheap Inertial Measurement Unit High Precision MEMS Inertial Navigation Vehicle Navigation Voltage 3.0~3.6V,One SPI 15MHz from wholesalers
    • Buy cheap Inertial Measurement Unit High Precision MEMS Inertial Navigation Vehicle Navigation Voltage 3.0~3.6V,One SPI 15MHz from wholesalers

    Inertial Measurement Unit High Precision MEMS Inertial Navigation Vehicle Navigation Voltage 3.0~3.6V,One SPI 15MHz

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    Brand Name : Kacise
    Model Number : KSIMU16495
    Certification : certificate of explosion-proof, CE
    Payment Terms : T/T, Western Union, MoneyGram
    Supply Ability : 1000 Pieces per Week
    Delivery Time : 5-8 working days
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    Inertial Measurement Unit High Precision MEMS Inertial Navigation Vehicle Navigation Voltage 3.0~3.6V,One SPI 15MHz

    Product Description:

    Inertial measurement Unit KSIMU16495 is a domestic inertial measurement equipment with high performance, small size and high overload resistance. Gyroscope zero bias stability 0.5°/h (Allan), accelerometer zero bias stability 10µg (Allan). It can be used for precise navigation, control and dynamic measurement of weapons. This series of products adopts high-precision MEMS inertial devices, with high reliability and high robustness, and can accurately measure the angular velocity and acceleration information of the moving carrier in harsh environments.

    The inertial measurement unit KSIMU16495 with built-in three-axis gyro and three-axis accelerometer is used to measure the carrier's three-axis angular rate and three-axis acceleration. Through the serial port according to the convention communication protocol output error compensation (including temperature compensation, installation misalignment Angle compensation, nonlinear compensation, etc.) gyroscope, accelerometer data, and built-in three-axis magnetic sensor, pressure sensor.


    Features:

    ● High precision MEMS inertial navigation

    ● Support dynamic fast alignment

    ● High bandwidth, high data update rate

    ● 1 channel SPI

    ● Small size, light weight

    ● Solid and reliable

    ● Fully compatible with a foreign 10 degrees of freedom inertial measurement system


    Technical Parameters:

    ParameterTest conditionMINTYPMAXUints
    Power supply parameter
    Voltage3.03.33.6V
    Power dissipation1.5W
    RippleP-P100mV
    Product performance
    GyroscopeRange±400±450deg/s
    zero-bias stabilityAllan0.8deg /h
    random walk0.06deg /√h
    Zero Bias Repeatability−40°C ≤ TA ≤ +85°C0.10.2deg/s
    Scale factor repeatability−40°C ≤ TA ≤ +85°C0.11%
    Scale factor nonlinearityFS=450 º/s0.10.2%FS
    Bandwidth400Hz
    AccelerometerRange±10g
    zero-bias stabilityAllan0.01mg
    random walk0.020.02m/s/√h
    Zero Bias Repeatability−40°C ≤ TA ≤ +85°C±2mg
    Scale factor repeatability−40°C ≤ TA ≤ +85°C0.51%
    Scale factor nonlinearity0.1%FS
    Bandwidth200Hz
    MagnetometerDynamic measuring range±2.5gauss
    Resolution120uGauss
    Noise density50uGauss
    Bandwidth200Hz
    BarometerPressure range4501100mbar
    Resolution0.1mbar
    Absolute measurement accuracy1.5mbar
    Communication interfaceOne SPIBaud rate15MHz
    Structural characteristicsSize44×47×14mmSize
    Weight50gWeight
    reliabilityMTBF20000h
    continuous working hours120h
    Environment
    Operating temperature-4075
    storage temperature-4585
    vibration10~2000Hz,3g
    Impact30g,11ms
    Overload(Half-sine 0.5msec)1000g

    Dimensions:

    Inertial Measurement Unit High Precision MEMS Inertial Navigation Vehicle Navigation Voltage 3.0~3.6V,One SPI 15MHz


    Coordinate System Definition:


    The coordinate system of the gyroscope and accelerometer is defined as shown in the figure below, with the arrow direction being positive.


    Read and Write Data:

    The KSIMU16495 is an automatic sensor system that automatically activates when an active power supply is present. After completing the initialization process, it begins sampling, processing, and loading calibrated sensor data into the output register, which can be accessed through the SPI port. The SPI port is usually connected to the compatible port of the embedded processor, the connection diagram is shown in the following 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 register, the pin becomes high level.



    Common Host Processor SPI Settings:

    Processor SettingsExplain
    HostKSIMU16495 is used as a slave machine
    SCLK ≤ 15 MHzMaximum serial clock rate
    SPI Mode 3CPOL = 1 (polarity),CPHA = 1 (phase position)
    MSB priority modeOrder
    16-bit modeShift register/data length

    SPI Communication:

    If the previous command is a read request, the SPI port supports full-duplex communication, and the external processor can write to DIN while reading the DOUT, as shown below.

    SPI read-write timing

    Read sensor data

    KSIMU16495 automatically starts and activates page 0 for data register access. After accessing any other pages, 0x00 should be written to the PAGE_ID register (DIN = 0x8000) to activate page 0, ready 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 contents of the register 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 irrelevant bits, but SPI needs the full 16 SCLKS to receive the request. The following figure shows two successive 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 register.


    Example of SPI read operation

    User register memory mapping (N/A means not applicable)

    R/WPAGE_IDAddressDefaultRegister description
    R/W0x000x000x00Page identity
    R0x000x0EN/ATemperature
    R0x000x10N/AX-axis gyroscope output, low byte
    R0x000x12N/AX-axis gyroscope output, high byte
    R0x000x14N/AY-axis gyroscope output, low byte
    R0x000x16N/AY-axis gyroscope output, high byte
    R0x000x18N/AZ-axis gyroscope output, low byte
    R0x000x1AN/AZ-axis gyroscope output, high byte
    R0x000x1CN/AX-axis accelerometer output, low byte
    R0x000x1EN/AX-axis accelerometer output, high byte
    R0x000x20N/AY-axis accelerometer output, low byte
    R0x000x22N/AY-axis accelerometer output, high byte
    R0x000x24N/AZ-axis accelerometer output, low byte
    R0x000x26N/AZ-axis accelerometer output, high byte
    R0x000x28N/AX-axis magnetic, high byte
    R0x000x2AN/AY-axis magnetic, high byte
    R0x000x2CN/AZ-axis magnetic, high byte
    R0x000x2EN/AAir pressure output, low byte
    R0x000x30N/AAir pressure output, low byte
    R/W0x030x000x00Page identity
    R/W0x030x060x000DControl, I/O pins, function definition
    R/W0x030x080x00X0Control, I/O pins, universal
    R/W0x040x000x00Page identity
    R0x040x20/serial number

    transformation formula

    Current temperature = 25+ TEMP OUT*0.00565

    X_GYRO_OUTX_GYRO_LOW
    X axis gyro example1LSB=0.02°/SThe weight of the MSB is 0.01°/S, and the weight of the subsequent bits is half that of the previous bits
    0.02*X_GYRO_OUT0.01*MSB+0.005*.......

    Y-axis Z-axis gyro is calculated in a similar way to X-axis gyro.

    X_ACCL_OUTX_ACCL_LOW
    X axis accelerometer example1LSB=0.8mgThe weight of MSB is 0.4mg, and the weight of each subsequent bit is half that of the previous bit
    0.8*X_ACCL_OUT0.4*MSB+0.2*.......

    Y-axis Z-axis accelerometer is calculated in a similar way to X-axis accelerometer.

    X_MAGN_OUT
    X-axis magnetometer1LSB=0.1mGauss
    0.1*X_MAGN_OUT

    Y-axis Z-axis magnetometer is calculated in a similar way to the X-axis magnetometer

    BAROM_OUTBAROM_LOW
    Barometric example1LSB=40ubarThe weight of MSB is 20ubar, and the weight of each subsequent bit is half that of the previous bit
    40*BAROM_OUT20*MSB+10*.......

    Note: Gyroscope, accelerometer, magnetometer is divided into high 16bit and low 16bit, respectively calculated to add the final result


    Electrical Interface:




    Pin numbernametypedescribe
    10,11,12VDDPower
    13,14,15GNDPower Ground
    7DIO1Input/OutputUniversal I/O, configurable
    9DIO2Input/Output
    1DIO3Input/Output
    2DIO4Input/Output
    3SPI-CLKInputThe SPI master/slave mode is configurable. The default mode is slave
    4SPI-MISOOutput
    5SPI-MOSIInput
    6SPI-CSInput
    8RSTInputRestoration
    23VDDRTCPower supply/
    16~21,24NCSpare pinManufacturer's reservation

    Quality Inertial Measurement Unit High Precision MEMS Inertial Navigation Vehicle Navigation Voltage 3.0~3.6V,One SPI 15MHz for sale
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