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Miniature Adis16488 MEMS Inertial Measurement Unit Sensor with SPI Output

Name: Miniature Adis16488 MEMS Inertial Measurement Unit Sensor with SPI Output
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: 16488HA
Price: 3,003.00 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	16488HA
MOQ:	1
Price:	Negotiable
Payment Terms:	T/T
Supply Ability:	200/MONTH

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Zero-bias Instability:

0.3º/h

Bias Repeatability:

≤5°/h

Bandwidth:

250 Hz

Angle Random Walk:

0.15°/√h

Acc Range:

±20g

Acc Bias Stability:

0.07 Mg

Packaging Details:

Sponge+ box

Supply Ability:

200/MONTH

Highlight:

dynamic fiber optic gyroscope sensor

UAV fiber optic gyroscope sensor

Product Description

Miniature ADIS16488 MEMS Inertial Measurement Unit Sensor with SPI Output

The 16488HA is a high-performance MEMS inertial measurement unit that combines a three-axis gyroscope and three-axis accelerometer to deliver precise angular rate and acceleration data. With measurement ranges up to ±450°/s and ±20 g, featuring 0.3°/h gyro zero-bias instability and 0.25 mg accelerometer bias, this unit ensures exceptional accuracy for inertial navigation applications.

The sensor includes onboard compensation for temperature variations (-45°C to 85°C), installation misalignment, and nonlinear effects. Its SPI communication interface operates at 8-15 MHz, with a compact design, 1.5 W power consumption, 250 Hz bandwidth, and 0.1% cross-axis coupling. Ideal for UAVs, industrial automation, autonomous vehicles, robotics, and mobile mapping systems.

Technical Specifications

Gyroscope Performance

Parameter	Test Conditions	Typical	Maximum	Unit
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 Performance

Parameter	Test Conditions	Typical	Maximum	Unit
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

Parameter	Test Conditions	Typical	Maximum	Unit
Communication Interface	1-way SPI	8	15	MHz
Voltage	Direct current	3.3		V
Power consumption		1.5	1.5	W
Ripple	P-P	48±2	100	mV

Environmental Specifications

Parameter	Test Conditions	Minimum	Typical	Maximum	Unit
Operating temperature		-45		85	℃
Storage temperature		-55		85	℃

Product Diagrams

Outline Drawing

Connector Diagram

Axial Direction Diagram

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

Gyro North Finder

Magnetometer Sensor

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

Gyro North Finder

Magnetometer Sensor

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Miniature Adis16488 MEMS Inertial Measurement Unit Sensor with SPI Output

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