ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS

Price	2000$
MOQ	1
Delivery Time	1 Week for sample
Brand	Firepower
Place of Origin	China
Model Number	16488HA
Packaging Details	BOX+Sponge
Payment Terms	L/C,D/A,D/P,T/T,Western Union
Supply Ability	500/month

Product Details

Product Specification

Place of Origin	China	Accelerometer bias stability	0.07mg
Random walk	0.15º/√h	Packaging Details	BOX+Sponge
Measuring range	±450°/s	Model Number	16488HA
Supply Ability	500/month	Accelerometer Range	±20g
Bandwidth (-3dB)	250Hz	Brand Name	Firepower
Payment Terms	L/C,D/A,D/P,T/T,Western Union	Price	2000$
Delivery Time	1 Week for sample	Minimum Order Quantity	1
Scale factor repeatability	100ppm	Voltage	3.3V
Bias instability	0.3°/h

Product Description

ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS

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) is a complete inertial sensing solution that combines a three-axis gyroscope and three-axis accelerometer in a compact package. This tactical-grade MEMS IMU precisely measures three-axis angular rates, linear accelerations, and dynamic parameters with advanced error compensation for high-accuracy data output.

Core Features

Comprehensive Motion Sensing: Simultaneously captures 3D angular velocity (gyroscopes) and acceleration (accelerometers) for complete motion tracking
Advanced Error Compensation: Implements temperature drift compensation, mounting misalignment calibration, and nonlinearity correction to minimize systematic errors
Digital Interface: Provides compensated data through industry-standard SPI communication protocol for easy system integration

Ideal for demanding applications including autonomous vehicles, robotics, and aerospace systems, the ADIS16488HA delivers reliable performance for inertial navigation and attitude control through its integrated hardware and intelligent error mitigation.

Technical Specifications

Parameter	Test Conditions	Min	Typical	Max	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		%
Electrical Characteristics
Voltage	Direct current		3.3		V
Power consumption			1.5	1.5	W
Ripple	P-P		48±2	100	mV
Environmental Specifications
Operating temperature		-45		85	℃
Storage temperature		-55		85	℃