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Next-Generation 10-Axis Inertial Measurement Unit for Precision Navigation

Name: Next-Generation 10-Axis Inertial Measurement Unit for Precision Navigation
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: 16488HB
Price: 500 USD
Availability: InStock

Nazwa marki:	FIREPOWER
Numer modelu:	16488HB
MOQ:	1
Cena £:	500$
Warunki płatności:	L/C, T/T
Zdolność do zaopatrzenia:	500/miesiąc

Szczegółowe informacje

Opis produktu

Szczegółowe informacje

Miejsce pochodzenia:

Chiny

Dynamiczny zakres pomiaru:

500/2000°/s

Stabilność odchylenia żyroskopowego:

0,8°/godz

Przypadkowy spacer:

0,15°/√h

Zakres akcelerometru:

16/200g

Ogólne wymiary:

47×44×14

Interfejs:

CAN/SPI

Szczegóły pakowania:

gąbka + karton

Możliwość Supply:

500/miesiąc

Podkreślić:

10-axis IMU for precision navigation

inertial measurement unit with gyro

high-accuracy IMU accelerometer sensor

Opis produktu

Next-Generation 10-Axis Inertial Measurement Unit for Precision Navigation

Product Overview

The 16488HB IMU features built-in high-performance MEMS sensors that deliver exceptional motion sensing capabilities. Advanced temperature calibration and compensation algorithms ensure high accuracy in dynamic environments. This unit serves as an ideal alternative to the Adis 16497, offering superior performance for unmanned motion carriers and mapping systems.

Product Features

Three-axis digital gyroscope: ±2000°/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: 2.5 gauss
Digital barometer: 300mbar ~ 1100mbar
High reliability: MTBF 20,000 hours
Guaranteed accuracy within full temperature range (-40℃ to +80℃): Built-in high-performance temperature calibration and compensation algorithm
Vibration resistance: Suitable for operation under strong vibration (6.06 G, 20-2000 Hz)
Impact resistance: Suitable for working under large impact conditions (1000 G, 0.5ms)

Technical Specifications

Parameter	Test Conditions	Min Value	Typical Value	Max 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℃ to +70℃, constant temperature), Z-axis		3		°/h
Zero bias stability	10s average (-40℃ to +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 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	10s average (-40℃ to +70℃, constant temperature)		0.4		mg
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 initiated on a daily basis			0.8		mg
Zero-bias temperature coefficient		0.05	0.1		mg/℃
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	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
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			474414		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℃ to +70℃

②: Vibration condition is 6.06 G, 20Hz to 2000Hz

Outline Drawing

Tagi:

Czujnik żyroskopowy akcelerometru

Żyroskop akcelerometru IMU

Kwarcowy akcelerometr giętki

żyroskop światłowodowy

System nawigacji inercyjnej

Wyszukiwarka północy żyroskopu

Czujnik magnetometru

Czujnik żyroskopowy akcelerometru

Żyroskop akcelerometru IMU

Kwarcowy akcelerometr giętki

żyroskop światłowodowy

System nawigacji inercyjnej

Wyszukiwarka północy żyroskopu

Czujnik magnetometru

szczegółowe informacje o produktach

Next-Generation 10-Axis Inertial Measurement Unit for Precision Navigation

Next-Generation 10-Axis Inertial Measurement Unit for Precision Navigation

10-axis IMU for precision navigation

inertial measurement unit with gyro

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Akcelerometr IMU z kompensacją temperatury Żyroskop 16488-C 3-osiowy

Kompaktowy i niskiej wagi czujnik inercyjny IMU

Gyrometr przyspieszacz IMU z wysoką zdolnością do dostosowania się do środowiska