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Light Weight Inertial Measure Unit 6 Axis Inertial Sensor With Wide Range

Name: Light Weight Inertial Measure Unit 6 Axis Inertial Sensor With Wide Range
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
Price:	negotiable
Payment Terms:	L/C,T/T
Supply Ability:	500/Month

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Certification:

Gyro Range:

±500/s

Gyro Zero Bias Stability:

0.8 °/h

Acc Range:

±16g

Acc Zero Bias Stability:

0.06mg(Allan)

Random Walk:

0.15º/√h

Bandwidth (-3dB):

200Hz

Interface:

1 Channel SPI/UART/CAN

Scale Factor Repeatability:

0.1%

Packaging Details:

Sponge/Box

Supply Ability:

500/Month

Highlight:

6 Axis Inertial Measure Unit

Light Weight Inertial Measure Unit

Wide Range Inertial Measure Unit

Product Description

Light Weight Inertial Measure Unit 6 Axis Inertial Sensor With Wide Range

The 16488HB multi-degree-of-freedom inertial measurement unit is a complete inertial system featuring built-in three-axis gyroscope, three-axis accelerometer, three-axis magnetometer, and pressure sensor. This advanced unit measures critical carrier parameters including three-axis angle rate, acceleration, three-axis magnetic field, and air pressure. All output data is delivered through SPI communication protocol after comprehensive error compensation, including temperature compensation, installation misalignment angle compensation, and nonlinear compensation.

Technical Specifications

Gyroscope Specifications

Parameter	Test Conditions	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	Zero-bias change in full temperature range, Z-axis ①	±0.02		°/s
Zero Bias	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
Effect 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	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 Specifications

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	Zero bias range		2		mg
Zero Bias	Change of zero bias within the whole temperature range, peak-to-peak value ①		4		mg
Repeatability of Successive Starts			0.5		mg
Repeatability Initiated on Daily Basis			0.8		mg
Zero-bias Temperature Coefficient		0.05	0.1		mg/℃

Dimensions

Notes:
① Zero bias change over full temperature range
② Vibration influence measurement

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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