Sign In | Join Free | My burrillandco.com
Home > IMU Accelerometer Gyro >

10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488

Shenzhen Fire Power Control Technology Co., LTD
Trust Seal
Verified Supplier
Credit Check
Supplier Assessment
Contact Now
    Buy cheap 10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488 from wholesalers
     
    Buy cheap 10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488 from wholesalers
    • Buy cheap 10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488 from wholesalers
    • Buy cheap 10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488 from wholesalers
    • Buy cheap 10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488 from wholesalers
    • Buy cheap 10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488 from wholesalers
    • Buy cheap 10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488 from wholesalers
    • Buy cheap 10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488 from wholesalers

    10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488

    Ask Lasest Price
    Brand Name : Firepower
    Model Number : 16488C
    Payment Terms : T/T,L/C
    Supply Ability : 1000pcs
    Delivery Time : 1 week
    • Product Details
    • Company Profile

    10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488

    Product Description


    16488C Multi-Degree-of-Freedom Inertial Measurement Unit (IMU) is a high-performance, fully integrated inertial system equivalent to the ADIS16488. It combines a three-axis gyroscope, three-axis accelerometer, three-axis magnetometer, and barometric pressure sensor in a compact module.

    This IMU provides accurate measurements of angular rate, linear acceleration, magnetic field, and air pressure for dynamic platforms such as autonomous vehicles, UAVs, robotics, and navigation systems.

    Featuring built-in error compensation (including temperature drift, misalignment, and nonlinear correction), the 16488C ensures exceptional stability and precision in harsh environments. Data is output via SPI or UART interface under standard communication protocols, enabling easy system integration and real-time motion sensing.


    Technical Parameters

    Parameter

    Test conditions

    Minimum value

    Typical value

    Maximum value

    Unit

    Gyroscope

    Dynamic measuring range

    Configurable

    ±450

    º/s

    Zero-bias instability

    Allan variance, better than

    5

    º/h

    Zero bias stability

    10s smooth, RMS, better than

    10

    º/h

    Zero bias in full temperature range

    -40 ℃ ~ 85 ℃, 10 s smooth,

    rms

    60

    º/h

    Random walk

    1σ

    0.26

    º/√h

    Zero-bias repeatability

    1σ

    20

    º/h

    Zero-bias acceleration sensitive

    20

    º/h/g

    Scale factor repeatability

    1σ

    200

    Ppm

    Scale factor nonlinearity

    FS=450 º/s

    200

    Ppm

    Bandwidth (-3dB)

    330

    Hz

    Cross coupling

    0.2

    %

    Accelerometer

    Dynamic measuring range

    Configurable

    ±20

    g

    Zero bias stability

    Allan variance

    0.07

    mg

    Zero bias in full temperature range

    -40 ℃ ~ 85 ℃, 10 s smooth,

    rms

    3

    mg

    Random walk

    0.029

    m/s/√h

    Zero-bias repeatability

    0.5

    mg

    Zero bias stability

    10s smooth, RMS, better than

    0.25

    mg

    Scale factor repeatability

    1σ

    500

    ppm

    Scale factor nonlinearity

    FS=10g

    500

    ppm

    Bandwidth (-3dB)

    250

    Hz

    Cross coupling

    0.2

    %

    Magnetometer

    Dynamic measuring range

    ±2.5

    gauss

    Sensitivity

    0.1

    mgauss/LSB

    Barometer

    Pressure range

    300

    1100

    mbar

    Sensitivity

    6.1 × 10-7

    mbar/LSB

    Electrical

    Characteristic

    Voltage

    Direct current

    3.3±0.15

    V

    Power consumption

    0.5

    W

    Ripple

    P-P

    100

    mV

    Weight

    48±2

    g

    Use

    Environment

    Operating temperature

    Scalable

    -45

    85

    Storage temperature

    -55

    85

    outline drawing


    10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488

    Quality 10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488 for sale
    Inquiry Cart 0
    Send your message to this supplier
     
    *From:
    *To: Shenzhen Fire Power Control Technology Co., LTD
    *Subject:
    *Message:
    Characters Remaining: (0/3000)