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Adis16488 Replacement Sensors lmu Accelerometer Gyro

Brand Name:	Firepower
Model Number:	16488HB
MOQ:	1
Price:	negotiable
Payment Terms:	L/C,T/T
Supply Ability:	500/Month

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Certification:

Acc Range:

±18g

Acc Zero Bias Stability:

0.07mg

Gyro Range:

±450°/s

Gyro Zero Bias Stability:

5.1 °/h

Random Walk:

0.26º/√h

Bandwidth (-3dB):

330Hz

Scale Factor Repeatability:

0.1%

Interface:

1 Channel SPI/UART/CAN

Packaging Details:

Sponge/Box

Supply Ability:

500/Month

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Product Description

ADIS16488 Replacement Sensors - IMU Accelerometer Gyro

The ADIS16488C multi-degree-of-freedom inertial measurement unit is a complete inertial system featuring a built-in three-axis gyroscope, three-axis accelerometer, three-axis magnetometer, and pressure sensor. This advanced system measures critical carrier parameters including three-axis angle rate, acceleration, three-axis magnetic field, and air pressure. All output data is provided after comprehensive error compensation (including temperature compensation, installation misalignment angle compensation, and nonlinear compensation) through the SPI communication protocol.

Technical Specifications

Gyroscope Parameters

Parameter	Test Conditions	Minimum	Typical	Maximum	Unit
Dynamic Measuring Range		500		2000	°/s
Zero Bias Stability	Allan variance, Z-axis		0.8		°/h
Zero Bias Stability	Allan variance, X and Y axis		1.6		°/h
Zero Bias Stability	10 s average (-40℃ ~ +70℃, constant temperature), Z-axis		3		°/h
Zero Bias Stability	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	Zero-bias range, X-axis and Y-axis		±0.2		°/s
Zero Bias Change	Full temperature range, Z-axis		±0.02		°/s
Zero Bias Change	Over temperature, X and Y axis		±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
Day-by-day Start Repeatability	X-axis and Y-axis		0.009		°/s
Effect of Linear Acceleration on Bias			0.002		°/s/g
Influence of Vibration on Zero Bias	Change before and after vibration		0.002		°/s/g
Influence of Vibration on Zero Bias	Change before and during vibration		0.002		°/s/g
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 Parameters

Parameter	Test Conditions	Minimum	Typical	Maximum	Unit
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 Range			2		mg
Zero Bias Change	Full temperature range, peak-to-peak value		4		mg
Successive Start Repeatability			0.5		mg
Day-by-day Start Repeatability			0.8		mg
Zero-bias Temperature Coefficient		0.05	0.1		mg/℃

Dimensions

Packaging & Shipping

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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