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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 variancedeg /h
    Random walkdeg /√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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