products details

Home Products

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 IMU 10DOF MEMS Inertial Measurement Unit with Bulit-in 3-Axis Gyro, Accel, Mag & Pressure Sensor

Product Description

The 16488HA Inertial Measurement Unit (IMU) represents a cutting-edge inertial sensing solution, integrating a tri-axis gyroscope and tri-axis accelerometer into a unified, high-performance system. Engineered to precisely quantify a carrier’s three-dimensional angular velocities, linear accelerations, and derived dynamic parameters, this IMU leverages advanced error mitigation algorithms to deliver mission-critical accuracy across demanding operational scenarios.

Key technical highlights include:

Holistic Sensing Architecture:Simultaneous capture of 3D angular rate (via MEMS gyroscopes) and acceleration (via MEMS accelerometers), forming the backbone of motion tracking systems for both static and dynamic environments.
Multifaceted Error Calibration:Implements a suite of intelligent compensations—including temperature drift correction, mounting misalignment calibration, nonlinearity rectification, and cross-axis error mitigation—to eliminate systematic errors at the source.
Standardized Digital Interface:Transmits fully compensated data streams through an industry-standard SPI protocol, enabling seamless integration with host controllers while ensuring real-time response (<50ms) and low-latency data exchange.

Designed for applications requiring uncompromised motion accuracy—ranging from autonomous navigation systems to high-precision industrial robotics—the 16488HA balances hardware miniaturization with robust performance. Its -40°C to +85°C operational temperature range, combined with IP67 environmental protection, makes it suitable for deployments in harsh environments, while the 0.5°/h bias stability ensures cumulative errors remain negligible even over prolonged operational cycles.

Technical Parameters

Parameter		Test conditions	Minimum value	Typical value	Maximum value	Unit
Gyroscope	Dynamic measuring range			±450		º/s
	Zero-bias instability	Allan variance, better than		0.3		º/h
	Zero bias stability	10s smooth, RMS, better than		3		º/h
	Zero bias in full temperature range	-40 ℃ ~ 85 ℃, 10 s smooth, rms		20		º/h
	Random walk	1σ		0.15		º/√h
	Zero-bias repeatability	1σ		5		º/h
	Scale factor repeatability	1σ		100		ppm
	Scale factor nonlinearity	1σ		100		ppm
	Bandwidth (-3dB)			250		Hz
	Cross coupling			0.1		%
	Resolution			2		º/h
	Acceleration sensitivity			2		°/h/g
Accelerometer	Dynamic measuring range			±20		g
	Zero bias stability	Allan variance		0.07		mg

	Zero bias in full temperature range	-40 ℃ ~ 85 ℃, 10 s smooth, rms		3		mg
	Zero bias stability	10s smooth, RMS, better than		0.25		mg
	Random walk	1σ		0.029		m/s/√h
	Zero-bias repeatability	1σ		0.5		mg
	Scale factor repeatability	1σ		500		ppm
	Scale factor nonlinearity	FS=20g		500		ppm
	Bandwidth (-3dB)			250		Hz
	Cross coupling			0.1		%
Communication Interface	1-way SPI	Enter the clock frequency		8	15	MHz
Electrical characteristics	Voltage	Direct current		3.3		V
	Power consumption			1.5	1.5	W
	Ripple	P-P		48±2	100	mV
Use environment	Operating temperature		-45		85	℃
Use environment	Storage temperature		-55		85	℃

Outline Structure

ADIS16488 IMU10DOF MEMS Inertial Measurement Unit with Bulit-in 3-Axis Gyro, Accel, Mag & Pressure Sensor 0

ADIS16488 IMU10DOF MEMS Inertial Measurement Unit with Bulit-in 3-Axis Gyro, Accel, Mag & Pressure Sensor 1

ADIS16488 IMU10DOF MEMS Inertial Measurement Unit with Bulit-in 3-Axis Gyro, Accel, Mag & Pressure Sensor 2

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

products details

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 IMU

Mag & Pressure Sensor IMU

ADIS16488 IMU Accelerometer Gyro

FOG IMU Inertial Measurement Unit

MEMS Small Inertial Measurement Unit

Stim300 IMU Accelerometer Gyro Sensor Factory Supply

Lightweight 6-axis Inertial Measurement Unit Accelerometer Gyroscope Sensor

Temperature Compensated IMU Accelerometer Gyro 16488-C 3 axis

Compact and Low Weight IMU Inertial Sensor Inertial Measurement Unit

IMU Accelerometer Gyro With High Environmental Adaptability

6 Axis IMU Accelerometer Gyro Inertial Measure Unit Low Cost

Three-Axis Gyro Accelerometer Integrated Inertial Measurement Unit with RS422 Output

Advanced MEMS Inertial Measurement Unit Sensor with 0.2° Bias Honeywell HG4930C IMU