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Low Dift Gyroscope Accelerometer Inertial Measurement Unit IMU

Name: Low Dift Gyroscope Accelerometer Inertial Measurement Unit IMU
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)

Interface:

1 Channel SPI/UART/CAN

Bandwidth (-3dB):

330Hz

Random Walk:

0.15º/√h

Power Consumption:

0.6W

Packaging Details:

Sponge/Box

Supply Ability:

500/Month

Highlight:

High performance IMU

Inertial Measurement Unit IMU

Gyroscope Accelerometer IMU

Product Description

Low Dift Gyroscope Accelerometer Inertial Measurement Unit IMU

Product Description

The 16488HB multi-degree-of-freedom inertial measurement unit is a complete inertial system with a built-in three-axis gyroscope, a three-axis accelerometer, a three-axis magnetometer and a pressure sensor for measuring the three-axis angle of the carrier parameters such as rate, acceleration, three-axis magnetic field, air pressure, etc., output data after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation, etc.) according to the communication protocol through SPI.

Three-axis digital gyroscope:

A) ± 2000º/s dynamic measurement range;

B) Zero bias stability: 3 °/H (GJB, 10S, Z-axis), 0.8 °/H (ALLAN, Z-axis);

2) Triaxial digital accelerometer:

A) ± 200g dynamic measurement range;

B) Zero bias stability: 0.4mg (GJB, 10S), 0.06mg (ALLAN);

3) Triaxial digital magnetometer: 2.5g auss

4) Digital barometer: 300mbar ~ 1100mbar

5) High reliability: MTBF 20000h;

6) Guaranteed accuracy within the full temperature range (-40 ℃ ~ + 80 ℃):

built-in high-performance temperature calibration and compensation algorithm;

7) Suitable for operation under strong vibration (6.06 G, 20 ~ 2000 Hz);

8) Suitable for working under large impact conditions (1000 G, 0.5ms);

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/℃

Dimension

Low Dift Gyroscope Accelerometer Inertial Measurement Unit IMU 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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