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9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation

    Buy cheap 9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation from wholesalers
     
    Buy cheap 9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation from wholesalers
    • Buy cheap 9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation from wholesalers
    • Buy cheap 9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation from wholesalers
    • Buy cheap 9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation from wholesalers
    • Buy cheap 9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation from wholesalers
    • Buy cheap 9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation from wholesalers
    • Buy cheap 9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation from wholesalers

    9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation

    Ask Lasest Price
    Brand Name : Firepower
    Model Number : 16488HA
    Certification : Military standard
    Price : negotiable
    Payment Terms : T/T
    Supply Ability : 50/month
    Delivery Time : 20 days for sample
    • Product Details
    • Company Profile

    9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation

    ADIS16488HA is a compact, lightweight MEMS IMU with three-axis gyroscope and accelerometer, measuring ±450°/s angular rate and ±20 g acceleration. Zero-bias instability is 0.3°/h for the gyro and 0.25 mg for the accelerometer, with minimal random walk and 100–500 ppm scale factor linearity. Temperature, misalignment, and nonlinear error compensation ensure reliable performance from -45~85 °C. SPI communication at 8–15 MHz, 1.5 W power consumption, 250 Hz bandwidth, and 0.1 % cross-coupling make it ideal for UAVs, robotics, industrial automation, mobile mapping, and precision navigaion systems.



    Technical Parameters

    Parameter

    Test conditions

    Minimum value

    Typical value

    Maximum value

    Unit

    Gyroscope

    Dynamic measuring range

    ±450

    º/s

    Zero-bias instability

    Allan variance, better than

    0.3

    º/h

    Zero bias stability

    10s smooth, RMS, better than

    3

    º/h

    Zero bias in full temperature range

    -40 ℃ ~ 85 ℃, 10 s smooth,

    rms

    20

    º/h

    Random walk

    0.15

    º/√h

    Zero-bias repeatability

    5

    º/h

    Scale factor repeatability

    100

    ppm

    Scale factor nonlinearity

    100

    ppm

    Bandwidth (-3dB)

    250

    Hz

    Cross coupling

    0.1

    %

    Resolution

    2

    º/h

    Acceleration sensitivity

    2

    °/h/g

    Accelerometer

    Dynamic measuring range

    ±20

    g

    Zero bias stability

    Allan variance

    0.07

    mg

    Zero bias in full temperature range

    -40 ℃ ~ 85 ℃, 10 s smooth,

    rms

    3

    mg

    Zero bias stability

    10s smooth, RMS, better than

    0.25

    mg

    Random walk

    0.029

    m/s/√h

    Zero-bias repeatability

    0.5

    mg

    Scale factor repeatability

    500

    ppm

    Scale factor nonlinearity

    FS=20g

    500

    ppm

    Bandwidth (-3dB)

    250

    Hz

    Cross coupling

    0.1

    %

    Communication

    Interface

    1-way SPI

    Enter the clock frequency

    8

    15

    MHz

    Electrical characteristics

    Voltage

    Direct current

    3.3

    V

    Power consumption

    1.5

    1.5

    W

    Ripple

    P-P

    48±2

    100

    mV

    Use environment

    Operating temperature

    -45

    85

    Storage temperature

    -55

    85

    outline drawing

    Connector


    axial direction

    Quality 9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation for sale
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