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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 Bulit-in 3-Axis Gyro, Accel, Mag & Pressure Sensor
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: 16488HA
Price: 2000 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	16488HA
MOQ:	1
Price:	2000$
Payment Terms:	L/C,D/A,D/P,T/T,Western Union
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

China

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

Packaging Details:

BOX+Sponge

Supply Ability:

500/month

Highlight:

ADIS16488 IMU

Mag & Pressure Sensor IMU

Product Description

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

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

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

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