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Lightweight MEMS IMU for UAV Flight Control and Stabilization

Shenzhen Fire Power Control Technology Co., LTD
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    Buy cheap Lightweight MEMS IMU for UAV Flight Control and Stabilization from wholesalers
     
    Buy cheap Lightweight MEMS IMU for UAV Flight Control and Stabilization from wholesalers
    • Buy cheap Lightweight MEMS IMU for UAV Flight Control and Stabilization from wholesalers
    • Buy cheap Lightweight MEMS IMU for UAV Flight Control and Stabilization from wholesalers
    • Buy cheap Lightweight MEMS IMU for UAV Flight Control and Stabilization from wholesalers
    • Buy cheap Lightweight MEMS IMU for UAV Flight Control and Stabilization from wholesalers
    • Buy cheap Lightweight MEMS IMU for UAV Flight Control and Stabilization from wholesalers
    • Buy cheap Lightweight MEMS IMU for UAV Flight Control and Stabilization from wholesalers

    Lightweight MEMS IMU for UAV Flight Control and Stabilization

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    Brand Name : Firepower
    Model Number : 16488D
    Payment Terms : T/T,L/C
    Supply Ability : 1000/month
    Delivery Time : 10 days for sample
    Price : 2000$
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    Lightweight MEMS IMU for UAV Flight Control and Stabilization

    Overview

    The 16488D is a high-performance inertial measurement unit that is precisely calibrated over the full temperature range to meet performance requirements under varying conditions. Built-in three-axis gyroscope and three-axis accelerometer are used to measure the three-axis angular rate, acceleration and other parameters of the carrier, and output the data after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation, etc.) through SPI according to the communication protocol.

    Performance indicators

    The specific performance index configuration of 16488D is shown in Table 1:

    Table 1 Performance index

    Parameter

    Test conditions

    Minimum value

    Typical value

    Maximum value

    Unit

    Gyroscope

    Dynamic measuring range

    ±500

    º/s

    Zero-bias instability

    Allan variance

    1

    º/h

    Zero bias stability

    1s smooth, RMS

    7

    º/h

    Zero bias in full temperature range

    -40 ℃ ~ 85 ℃, 10 s smoothing, RMS

    0.007

    º/s

    Random walk

    0.13

    º/√h

    Zero-bias repeatability

    5

    º/h

    Output noise

    No filtering, RMS

    0.02

    º/s

    Scale factor nonlinearity

    0.01

    %

    Scale factor

    FS=500 º/s

    524.287

    LSB/°/sec

    Bandwidth (-3dB)

    150

    280

    Hz

    Cross coupling

    0.05

    %

    Acceleration sensitivity

    10.7

    °/h/g

    Resonant frequency

    19k

    Hz

    Accelerometer

    Dynamic measuring range

    ±16

    g

    Zero bias stability

    Allan variance

    18

    ug

    Zero bias in full temperature range

    -40 ℃ ~ 85 ℃, 10 s smoothing, RMS

    0.3

    mg

    Random walk

    0.015

    m/s/√h

    Zero-bias repeatability

    1

    mg

    Output noise

    No filtering, RMS

    0.2

    mg

    Scale factor

    16383

    g/LSB

    Bandwidth (-3dB)

    150

    280

    Hz

    Cross coupling

    0.05

    %

    Magnetometer

    Range

    2(8)

    guass

    Resolution

    0.1

    mg

    Barometer

    Range

    260

    1260

    hPa

    Resolution

    4096

    LSB/hPa

    Temperature

    Scale factor

    0.019

    °C/LSB

    Communication interface

    1-way SPI

    Enter the clock frequency

    6

    12

    MHz

    Electrical characteristics

    Voltage

    Direct current

    3

    3.3

    3.6

    V

    Power consumption

    1

    W

    Ripple

    P-P

    50

    mV

    Use environment

    Operating temperature

    Scalable

    -40

    85

    Storage temperature

    -55

    105

    Impact

    2000g

    3.Outline and structure

    Lightweight MEMS IMU for UAV Flight Control and Stabilization

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