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ADIS16488 IMU10DOF MEMS Inertial Measurement Unit with Bulit-in 3-Axis Gyro, Accel, Mag & Pressure Sensor

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ADIS16488 IMU10DOF MEMS Inertial Measurement Unit with Bulit-in 3-Axis Gyro, Accel, Mag & Pressure Sensor

Brand Name : Firepower

Model Number : 16488HA

Place of Origin : China

MOQ : 1

Price : 2000$

Payment Terms : L/C,D/A,D/P,T/T,Western Union

Supply Ability : 500/month

Delivery Time : 1 Week for sample

Packaging Details : BOX+Sponge

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

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ADIS16488 IMU 10DOF MEMS Inertial Measurement Unit
Built-in 3-Axis Gyroscope, Accelerometer, Magnetometer & Pressure Sensor
Key Specifications
Attribute Value
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) represents a cutting-edge inertial sensing solution, integrating tri-axis gyroscope and accelerometer functionality into a unified, high-performance system. Engineered for precise measurement of three-dimensional angular velocities, linear accelerations, and derived dynamic parameters, this IMU delivers mission-critical accuracy through advanced error mitigation algorithms.

Key Features
  • Holistic Sensing Architecture: Simultaneous capture of 3D angular rate (via MEMS gyroscopes) and acceleration (via MEMS accelerometers) for comprehensive motion tracking in both static and dynamic environments.
  • Advanced Error Calibration: Implements intelligent compensation for temperature drift, mounting misalignment, nonlinearity, and cross-axis errors to eliminate systematic inaccuracies.
  • Standardized Digital Interface: SPI protocol ensures seamless integration with host controllers while maintaining real-time response (<50ms) and low-latency data exchange.
  • Robust Environmental Performance: Operational range of -40°C to +85°C with IP67 protection for harsh environment deployments.
  • Precision Engineering: 0.5°/h bias stability minimizes cumulative errors during prolonged operational cycles.
Technical Parameters
Parameter Test Conditions Min Typical Max Unit
Gyroscope Dynamic Range ±450 º/s
Zero-bias Instability Allan variance 0.3 º/h
Zero Bias Stability 10s smooth, RMS 3 º/h
Random Walk 1σ 0.15 º/√h
Scale Factor Repeatability 1σ 100 ppm
Bandwidth (-3dB) 250 Hz
Accelerometer Dynamic Range ±20 g
Accelerometer Zero Bias Stability Allan variance 0.07 mg
Voltage Direct current 3.3 V
Operating Temperature -45 85 ℃
Physical Dimensions
ADIS16488 IMU10DOF MEMS Inertial Measurement Unit with Bulit-in 3-Axis Gyro, Accel, Mag & Pressure Sensor ADIS16488 IMU10DOF MEMS Inertial Measurement Unit with Bulit-in 3-Axis Gyro, Accel, Mag & Pressure Sensor ADIS16488 IMU10DOF MEMS Inertial Measurement Unit with Bulit-in 3-Axis Gyro, Accel, Mag & Pressure Sensor

Note: Specifications subject to change without notice. Contact our technical team for application-specific performance verification.


Product Tags:

ADIS16488 IMU

      

Mag & Pressure Sensor IMU

      
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