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ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS

Shenzhen Fire Power Control Technology Co., LTD
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    Buy cheap ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS from wholesalers
     
    Buy cheap ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS from wholesalers
    • Buy cheap ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS from wholesalers
    • Buy cheap ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS from wholesalers
    • Buy cheap ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS from wholesalers

    ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS

    Ask Lasest Price
    Brand Name : Firepower
    Model Number : 16488HA
    Price : 2000$
    Payment Terms : L/C,D/A,D/P,T/T,Western Union
    Supply Ability : 500/month
    Delivery Time : 1 Week for sample
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    ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS

    ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS
    Key Specifications
    Measuring range
    ±450°/s
    Bias instability
    0.3°/h
    Random walk
    0.15º/√h
    Scale factor repeatability
    100ppm
    Bandwidth (-3dB)
    250Hz
    Accelerometer Range
    ±20g
    Accelerometer bias stability
    0.07mg
    Voltage
    3.3V
    Product Overview

    The ADIS16488HA Inertial Measurement Unit (IMU) is a complete inertial sensing solution that combines a three-axis gyroscope and three-axis accelerometer in a compact package. This tactical-grade MEMS IMU precisely measures three-axis angular rates, linear accelerations, and dynamic parameters with advanced error compensation for high-accuracy data output.

    Core Features
    • Comprehensive Motion Sensing: Simultaneously captures 3D angular velocity (gyroscopes) and acceleration (accelerometers) for complete motion tracking
    • Advanced Error Compensation: Implements temperature drift compensation, mounting misalignment calibration, and nonlinearity correction to minimize systematic errors
    • Digital Interface: Provides compensated data through industry-standard SPI communication protocol for easy system integration
    Ideal for demanding applications including autonomous vehicles, robotics, and aerospace systems, the ADIS16488HA delivers reliable performance for inertial navigation and attitude control through its integrated hardware and intelligent error mitigation.
    Technical Specifications
    ParameterTest ConditionsMinTypicalMaxUnit
    Gyroscope
    Dynamic measuring range±450º/s
    Zero-bias instabilityAllan variance, better than0.3º/h
    Zero bias stability10s smooth, RMS, better than3º/h
    Zero bias in full temperature range-40℃ ~ 85℃, 10 s smooth, rms20º/h
    Random walk0.15º/√h
    Zero-bias repeatability5º/h
    Scale factor repeatability100ppm
    Scale factor nonlinearity100ppm
    Bandwidth (-3dB)250Hz
    Cross coupling0.1%
    Resolution2º/h
    Acceleration sensitivity2°/h/g
    Accelerometer
    Dynamic measuring range±20g
    Zero bias stabilityAllan variance0.07mg
    Zero bias in full temperature range-40℃ ~ 85℃, 10 s smooth, rms3mg
    Zero bias stability10s smooth, RMS, better than0.25mg
    Random walk0.029m/s/√h
    Zero-bias repeatability0.5mg
    Scale factor repeatability500ppm
    Scale factor nonlinearityFS=20g500ppm
    Bandwidth (-3dB)250Hz
    Cross coupling0.1%
    Electrical Characteristics
    VoltageDirect current3.3V
    Power consumption1.51.5W
    RippleP-P48±2100mV
    Environmental Specifications
    Operating temperature-4585
    Storage temperature-5585
    Product Diagrams
    ADIS16488 IMU structural diagram showing component layout ADIS16488 IMU dimensional drawing with measurement specifications ADIS16488 IMU interface and connection diagram
    Quality ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS for sale
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