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Low Bias 16488 MEMS IMU Accelerometer Gyro With Built In GPS / BD Dual Mode

Shenzhen Fire Power Control Technology Co., LTD
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    Buy cheap Low Bias 16488 MEMS IMU Accelerometer Gyro With Built In GPS / BD Dual Mode from wholesalers
     
    Buy cheap Low Bias 16488 MEMS IMU Accelerometer Gyro With Built In GPS / BD Dual Mode from wholesalers
    • Buy cheap Low Bias 16488 MEMS IMU Accelerometer Gyro With Built In GPS / BD Dual Mode from wholesalers

    Low Bias 16488 MEMS IMU Accelerometer Gyro With Built In GPS / BD Dual Mode

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    Brand Name : Firepower
    Model Number : 16480C
    Certification : CE ROHS
    Price : negotiable
    Payment Terms : T/T,L/C
    Supply Ability : 500/month
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    Low Bias 16488 MEMS IMU Accelerometer Gyro With Built In GPS / BD Dual Mode

    Inertial Measurement Unit ADIS16488 Small Size And High Overload Resistance IMU

    Low Bias Stability IMU 16488 High Precision MEMS Inertial Devices With Built In GPS / BD Dual Mode Satellite R


    IMU16488B is a domestic inertial measurement unit with high performance, small size and high overload resistance.

    The gyro bias stability is 1.2 °/H (Allan) and the accelerometer bias stability is 50 µg (Allan). It can be used for precise

    navigation, control and dynamic measurement of weapons. This series of products adopt high-precision MEMS inertial

    devices, which have high reliability and high robustness, and can accurately measure the angular velocity and

    acceleration information of moving carriers in harsh environments.


    Product features:


    ※ High Precision MEMS Inertial Navigation ※ GPS/BD Dual Mode

    ※ Integrated navigation, AHRS, vertical gyro and other working modes

    ※ Support dynamic fast alignment ※ High bandwidth, 400Hz data update rate

    ※ External interface: 1-channel SPI and 1-channel UART

    ※ Support multiple external sensor combinations (odometer/DVL)

    ※ Small size, light weight ※ Strong and reliable

    ※ Fully compatible with a foreign 10-Dof inertial measurement system


    Main technical indicators




    Test conditions

    Minimum value

    Typical value

    Maximum value



    Measuring range




    Zero bias stabilityAllan variance



    deg /h
    Random walk



    deg /√h
    Zero-bias repeatability


    −40°C ≤ TA ≤ +85°C





    Scale factor repeatability

    Full temperature range

    −40°C ≤ TA ≤ +85°C





    Scale factor nonlinearityFS=450 º/s













    ±5


    Zero bias stability




    Random walk




    Zero-bias repeatability

    Full temperature range

    −40°C ≤ TA ≤ +85°C





    Scale factor repeatability

    Full temperature range

    −40°C ≤ TA ≤ +85°C





    Scale factor nonlinearity

    0.1


    0.2








    Hz 3dB

    Dynamic measuring range











    Noise density











    Pressure range










    Absolute measurement accuracy




    Externally based


    Inertial satellite

    Integrated navigation


    Heading accuracySingle GNSS, Maneuver Required, RMS



    Pitch and roll accuracyGNSS Valid, RMS



    GNSS invalid, unlimited time, RMS



    Position accuracyGNSS Valid, Single Point L1/L2, RMS



    Speed accuracyGNSS Valid, Single Point L1/L2, RMS



    Communication interface1-way SPIBaud rate



    1-way UARTBaud rate




    Electrical characteristics






    Power consumption










    Structural characteristics












    Use environmentOperating temperature




    Storage temperature







    1. ,3g





    1. ,11ms




    (Half-sine 0.5msec)










    Continuous working time





    IMU polarity definition

    3 gyros and 3 accelerometers is defined as shown in the figure below, and the direction of the arrow is positive.


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