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Miniature MEMS Inertial measurement Unit with with 3-Axis Gyroscope & Accelerometer for UAV

Name: Miniature MEMS Inertial measurement Unit with with 3-Axis Gyroscope & Accelerometer for UAV
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: 16488HB
Price: 600 USD
Availability: InStock

Brand Name:	FIREPOWER
Model Number:	16488HB
MOQ:	1
Price:	600$
Payment Terms:	D/A,T/T
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

China

Certification:

Dynamic Measuring Range:

500/2000°/s

Bias Stability:

0.8°/h

Angular Random Walk:

0.15°/ √hr

Bandwidth:

200Hz

Accelerometer Range:

16/200g

Accelerometer Bias Stability:

0.06mg

Size:

47×44×14mm

Weight:

50g

Packaging Details:

Carton+ Sponge

Supply Ability:

500/month

Product Description

Product Overview

The 16488HB inertial measurement unit combines cutting-edge MEMS technology with robust design to meet the demands of harsh industrial environments. It outputs 3 angular velocities and 3 accelerations, with a gyro dynamic range of ±2000º/s and accelerometer range of ±200g. With MTBF of 20000h and full-temperature accuracy guarantee, it’s the top choice for unmanned systems, mobile communication, and mapping.

Product Features

Three-axis digital gyroscope:
- ± 2000º/s dynamic measurement range;
- Zero bias stability: 3 °/H (GJB, 10S, Z-axis), 0.8 °/H (ALLAN, Z-axis);
Triaxial digital accelerometer:
- ± 200g dynamic measurement range;
- Zero bias stability: 0.4mg (GJB, 10S), 0.06mg (ALLAN);
Triaxial digital magnetometer: 2.5g auss
Digital barometer: 300mbar ~ 1100mbar
High reliability: MTBF 20000h;
Guaranteed accuracy within the full temperature range (-40 ℃ ~ + 80 ℃):
- built-in high-performance temperature calibration and compensation algorithm;
Suitable for operation under strong vibration (6.06 G, 20 ~ 2000 Hz);
Suitable for working under large impact conditions (1000 G, 0.5ms);

Field of Application

Unmanned motion carrier
Communication in motion
Surveying and mapping
Stabilizing platform

Product Indicators

16488HB Product Index

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, peak-to-peak value 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		°/s
	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

Parameter		Test conditions	Minimum value	Typical value	Maximum value	Unit
Magnetometer	Magnetic field range	Brg,xy		±13		gauss
	Magnetic field range	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
Barometer	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
	Sampling frequency	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
Structural characteristics	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
Reliability	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

Miniature MEMS Inertial measurement Unit with with 3-Axis Gyroscope & Accelerometer for UAV 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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