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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: 16488HB
Price: 3,003.00 USD
Availability: InStock

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

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Acc Range:

±16g

Gyro Range:

±500/2000º/s

Zero-bias Instability:

3º/h

Angular Random Walk:

0.15°/ √hr

Bandwidth:

200 Hz

Voltage:

3.3±0.15V

Weight:

50g

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 16488HB 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			500	2000	°/s
	Zero bias stability	Allan variance, Z-axis		0.8		°/h
		Allan variance, X and Y axis		1.6		°/h
		10 s average (-40 ℃ ~ + 70 ℃, constant temperature), Z-axis		3		°/h
		10 s average (-40 ℃ ~ + 70 ℃, constant temperature), X-axis and Y-axis		6		°/h
	Zero bias	Zero-bias range, Z-axis		±0.07		°/s
		Zero-bias range, X-axis and Y-axis		±0.2		°/s
		Zero-bias change in full temperature range, Z-axis ①		±0.02		°/s
		Zero Bias Change Over Temperature, X and Y Axis ①		±0.06		°/s
		Successive Start Repeatability, Z-axis		0.002
		Successive Start Repeatability, X-Axis and Y-Axis		0.006
		Day-by-day start repeatability, Z-axis		0.003		/s
		Start repetition day by day, X axis and Y axis		0.009		°/s
		Ffect of linear acceleration on bias		0.002		°/s/g
		Influence of vibration on zero bias, change before and after vibration ②		0.002		°/s/g
		Influence of vibration on zero bias, change before and during vibration ②		0.002		°/s/g
	Scale factor	Scale factor accuracy, Z-axis		0.3		%
		Scale Factor Accuracy, X and Y Axis		0.6		%
		Scale factor nonlinearity, Z-axis		0.01		%FS
		Scale Factor Nonlinearity, X and Y Axis		0.02		%FS
	Angular random walk			0.15		°/ √hr
	Noise density			0.001		°/s/ √Hz
	Resolution			3.052×10-7		/s/LSB
	Bandwidth			200		Hz
Accelerometer	Dynamic measuring range			16	200	g
	Zero bias stability	Allan variance		0.06		mg
	Zero bias stability	10 s average (-40 ℃ ~ + 70 ℃, constant temperature)		0.4		mg
	Zero bias	Zero bias range		2		mg
		Change of zero bias within the whole temperature range, peak-to-peak value ①		4		mg
		Repeatability of successive starts		0.5		mg
		Repeatability is initiated on a daily basis		0.8		mg
		Zero-bias temperature coefficient		0.05	0.1	mg/℃

	Scale factor	Scale factor accuracy		0.5		%
		Scale factor nonlinearity		0.1		%FS
	Speed random walk			0.029		m/s/ √hr
	Noise density			0.025		mg/ √Hz
	Resolution			1.221×10-8		g/LSB
	Bandwidth			200		Hz
Magnetometer	Magnetic field range	Brg,xy		±13		gauss
		Brg,z		±25		gauss
	Resolution			0.3		μT
	Heading accuracy	30 μT horizontal geomagnetic component, 25 ℃		±2.5		deg
	Dynamic measuring range			2.5		gauss
	Zero bias	Non-magnetic environment		15		mgausS
Barometer	Dynamic measuring range		300		1100	mbar
	Zero bias			4.5		mbar
Communication interface	1-way SPI	Baud rate			15	MHz
	1-Way C A N	Baud rate			1	MHz
	Sampling frequency	SPI		2460	2460	Hz
		CAN		200
Electrical characteristics	Voltage		3.0	3.3	3.6	V
	Power consumption				1.5	W
	Ripple	P-P			100	mV
	Settling time	From 0 V to 3. 3V			80	ms

Structural characteristics	Size		47×44×14		mm
	Weight		50		g
Use environment	Operating temperature	-40		70	℃
	Storage temperature	-45		75	℃
	Vibration		20~2000Hz, 6.06g
	Impact		1000g,0.5ms
Reliability	MTBF		20000		h
	Continuous working time		120		h
①: Calculate the zero deviation of the whole temperature change process, the temperature change rate is ≤ 1 ℃/min, and the temperature range is -40 ℃ ~ + 70 ℃ ②: Vibration condition is 6.06 G, 20Hz ~ 2000Hz

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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