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ADIS16488 analog IMU Accelerometer Gyro MEMS Inertial Measurement Unit

Brand Name:	Firepower
Model Number:	16488HB
MOQ:	1
Payment Terms:	T/T
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Certification:

CE ROHS

Product Name:

MEMS IMU

Bias Stability:

0.8°/h

Random Walk:

0.15°/ √hr

Bandwidth:

200Hz

Communication Interface:

SPI/CAN

Size:

47×44×14mm

Packaging Details:

sponge/box

Supply Ability:

500/month

Highlight:

Analog IMU Accelerometer Gyro

ADIS16488 IMU Accelerometer Gyro

MEMS Inertial Measurement Unit

Product Description

ADIS16488 analog sensor high performance MEMS IMU replace ADIS16488

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/℃

16488-HB is a domestic MEMS IMU used to replace ADIS16488. The product precision is better than ADIS16488. The version is optional, the size and appearance are exactly the same, and the communication protocol is the same.The version is optional, the size and appearance are exactly the same, and the communication protocol is the same. It is more convenient for users to change, providing users with professional product customization services.
ADIS16488 analog IMU Accelerometer Gyro MEMS Inertial Measurement Unit 0

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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