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10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488

Name: 10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: 16488C
Price: 3,003.00 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	16488C
MOQ:	1
Payment Terms:	T/T,L/C
Supply Ability:	1000pcs

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Acc Range:

±20g

Gyro Range:

±450º/s

Zero-bias Instability:

5º/h

Zero-bias Acceleration Sensitiv:

20º/h/g

Bandwidth:

330 Hz

Voltage:

3.3±0.15V

Weight:

48g

Magnetometer Sensitivity:

0.1mgauss/LSB

Packaging Details:

wooden box

Supply Ability:

1000pcs

Highlight:

Vibration 2 Axis Turntable

2 Axis Turntable Frame Based

Product Description

10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488

Product Description

The 16488C Multi-Degree-of-Freedom Inertial Measurement Unit (IMU) is a high-performance, fully integrated inertial system equivalent to the ADIS16488. It combines a three-axis gyroscope, three-axis accelerometer, three-axis magnetometer, and barometric pressure sensor in a compact module.

This IMU provides accurate measurements of angular rate, linear acceleration, magnetic field, and air pressure for dynamic platforms such as autonomous vehicles, UAVs, robotics, and navigation systems.

Featuring built-in error compensation (including temperature drift, misalignment, and nonlinear correction), the 16488C ensures exceptional stability and precision in harsh environments. Data is output via SPI or UART interface under standard communication protocols, enabling easy system integration and real-time motion sensing.

Key Features

10-axis inertial measurement system (gyro, accelerometer, magnetometer, barometer)
High-performance equivalent to ADIS16488
Built-in error compensation for temperature drift and misalignment
SPI and UART interface options
Compact, integrated design
Suitable for UAVs, autonomous vehicles, and robotics

Technical Parameters

Parameter	Test conditions	Minimum value	Typical value	Maximum value	Unit
Gyroscope
Dynamic measuring range	Configurable			±450	º/s
Zero-bias instability	Allan variance, better than		5		º/h
Zero bias stability	10s smooth, RMS, better than		10		º/h
Zero bias in full temperature range	-40 ℃ ~ 85 ℃, 10 s smooth, rms		60		º/h
Random walk	1σ		0.26		º/√h
Zero-bias repeatability	1σ		20		º/h
Zero-bias acceleration sensitive			20		º/h/g
Scale factor repeatability	1σ		200		Ppm
Scale factor nonlinearity	FS=450 º/s		200		Ppm
Bandwidth (-3dB)			330		Hz
Cross coupling			0.2		%
Accelerometer
Dynamic measuring range	Configurable			±20	g
Zero bias stability	Allan variance		0.07		mg
Zero bias in full temperature range	-40 ℃ ~ 85 ℃, 10 s smooth, rms		3		mg
Random walk	1б		0.029		m/s/√h
Zero-bias repeatability	1б		0.5		mg
Zero bias stability	10s smooth, RMS, better than		0.25		mg
Scale factor repeatability	1σ		500		ppm
Scale factor nonlinearity	FS=10g		500		ppm
Bandwidth (-3dB)			250		Hz
Cross coupling			0.2		%
Magnetometer
Dynamic measuring range			±2.5		gauss
Sensitivity			0.1		mgauss/LSB
Barometer
Pressure range		300		1100	mbar
Sensitivity			6.1 × 10-7		mbar/LSB
Electrical Characteristic
Voltage	Direct current		3.3±0.15		V
Power consumption			0.5		W
Ripple	P-P		100		mV
Weight			48±2		g
Use Environment
Operating temperature	Scalable	-45		85	℃
Storage temperature		-55		85	℃

Outline Drawing

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

products details

10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488

10-Axis Inertial Measurement Unit for UAV Attitude and Altitude Control Adis16488

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