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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

Name: ADIS16488 IMU10DOF MEMS Inertial Measurement Unit with Bulitin 3Axis Gyro Accel Mag amp Pressure Sensor
Brand: Firepower
Price: 2000 USD

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

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

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

Product Tags:

ADIS16488 IMU

Mag & Pressure Sensor IMU

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

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