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High Performance MEMS Inertial Measurement Unit IMU Sensor ADIS16488 Replacement

Name: High Performance MEMS Inertial Measurement Unit IMU Sensor ADIS16488 Replacement
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 Replacement IMU Sensor

ADIS16488 Inertial Measurement Unit

MEMS Inertial Measurement Unit

Product Description

High Performance MEMS Inertial Measurement Unit IMU Sensor ADIS16488 Replacement

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 16488HA Inertial Measurement Unit (IMU) is a fully integrated inertial sensing system that combines a three-axis gyroscope and a three-axis accelerometer within a compact module. It accurately measures three-axis angular velocity and linear acceleration of the host platform.

Advanced Error Compensation Features

Temperature compensation
Installation misalignment correction
Nonlinearity correction

The unit outputs high-precision inertial data via an SPI digital interface, following a standardized communication protocol, making it ideal for embedded applications requiring reliable motion sensing in dynamic environments.

Technical Specifications

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	℃
Storage temperature		-55		85	℃

Outline Structure

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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