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

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

Tactical Grade Inertial Measurement Unit

10‑DOF MEMS Inertial Measurement Unit

Product Description

ADIS16488 Inertial Sensor Tactical Grade10‑DOF MEMS Inertial Measurement Unit for INS

Product Description

The 16488HA Inertial Measurement Unit (IMU) stands as a comprehensive inertial sensing system, integrating a three-axis gyroscope and three-axis accelerometer within a single compact package. Designed to precisely measure the carrier's three-axis angular rates, linear accelerations, and related dynamic parameters, this IMU incorporates advanced error compensation algorithms to deliver highly accurate data.

Key features include:

Comprehensive Sensing:Simultaneously captures three-dimensional angular velocity (via gyroscopes) and acceleration (via accelerometers), forming the core of motion tracking systems.
Multi-Layer Compensation:Implements sophisticated error corrections, including temperature drift compensation, mounting misalignment calibration, nonlinearity correction, and more, to eliminate systematic errors.
Digital Interface:Outputs compensated data through an SPI communication protocol, adhering to industry-standard interfaces for seamless integration with control systems.

Ideal for applications requiring precise motion tracking—such as autonomous vehicles, robotics, or aerospace systems—the 16488HA ensures reliable performance by combining hardware integration with intelligent error mitigation, making it a robust solution for inertial navigation and attitude control

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 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS 0

ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS 1

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

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

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