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ADIS16495 Tactical Grade 10-DOF Inertial Measurement Unit for Inertial Navigation System

Name: ADIS16495 Tactical Grade 10-DOF Inertial Measurement Unit for Inertial Navigation System
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: 16488HB
Price: 600 USD
Availability: InStock

Markenbezeichnung:	FIREPOWER
Modellnummer:	16488HB
MOQ:	1
Preis:	600$
Zahlungsbedingungen:	D/a, t/t
Versorgungsfähigkeit:	500/Monat

Einzelheiten

Produktbeschreibung

Einzelheiten

Herkunftsort:

China

Zertifizierung:

Dynamischer Messbereich:

500/2000°/s

Biasstabilität:

0,8°/h

Angular Random Walk:

0,15°/√Std

Bandbreite:

200Hz

Beschleunigungsmesser-Strecke:

16/200g

Beschleunigungsmesser-Bias-Stabilität:

00,06 mg

Größe:

47×44×14mm

Gewicht:

50g

Verpackung Informationen:

Carton+-Schwamm

Versorgungsmaterial-Fähigkeit:

500/Monat

Produktbeschreibung

ADIS16495 Tactical Grade 10-DOF Inertial Measurement Unit for Inertial Navigation System

Product Overview

High-reliability MEMS IMU 16488HB integrates 3-axis gyroscope, accelerometer, magnetometer, and barometer for comprehensive motion sensing. Its exceptional zero bias stability (gyro 0.8°/h, accelerometer 0.06mg) and resistance to strong vibration (20~2000Hz, 6.06G) and impact (1000G, 0.5ms) make it perfect for unmanned motion carriers and industrial stabilization tasks.

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 full temperature range (-40℃ ~ +80℃): Built-in high-performance temperature calibration and compensation algorithm
Suitable for operation under strong vibration (6.06G, 20~2000Hz)
Suitable for working under large impact conditions (1000G, 0.5ms)

Field of Application

Unmanned motion carrier
Communication in motion
Surveying and mapping
Stabilizing platform

Product Specifications

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
Zero bias stability	Allan variance, X and Y axis		1.6		°/h
Zero bias stability	10s average (-40℃~+70℃, constant temperature), Z-axis		3		°/h
Zero bias stability	10s 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 in 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
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			0.002		°/s/g
Influence of vibration on zero bias, change before and during vibration			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
Dynamic measuring range			16	200	g
Zero bias stability	Allan variance		0.06		mg
Zero bias stability	10s 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			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
Magnetometer
Magnetic field range	Brg,xy		±13		gauss
Magnetic field range	Brg,z		±25		gauss
Resolution			0.3		μT
Heading accuracy	30μT 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
Zero bias			4.5		mbar
Communication Interface
1-way SPI	Baud rate			15	MHz
1-Way CAN	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 0V to 3.3V			80	ms
Structural Characteristics
Size			47×44×14		mm
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
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 6.06G, 20Hz~2000Hz

Outline Drawing

Tags:

Beschleunigungsmesser-Kreiselkompass-Sensor

IMU-Beschleunigungsmesser-Kreiselkompaß

Quarzbiegungsbeschleunigungsmesser

Faseroptikkreiselkompaß

Trägheitsnavigationsanlage

Kreiselkompass-Nordsucher

Magnetometer-Sensor

Beschleunigungsmesser-Kreiselkompass-Sensor

IMU-Beschleunigungsmesser-Kreiselkompaß

Quarzbiegungsbeschleunigungsmesser

Faseroptikkreiselkompaß

Trägheitsnavigationsanlage

Kreiselkompass-Nordsucher

Magnetometer-Sensor

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ADIS16495 Tactical Grade 10-DOF Inertial Measurement Unit for Inertial Navigation System

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