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10-Axis IMU Sensor ±0.8°/h Bias Stability Low Noise for Drone Attitude Control

Name: 10-Axis IMU Sensor ±0.8°/h Bias Stability Low Noise for Drone Attitude Control
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: 16488HB
Price: 500 USD
Availability: InStock

Наименование марки:	FIREPOWER
Номер модели:	16488HB
МОК:	1
цена:	500$
Условия оплаты:	Л/К, Т/Т
Способность к поставкам:	500/месяц

Подробная информация

Описание продукта

Подробная информация

Место происхождения:

Китай

Ряд волчка:

500/2000 º/с

Стабильность нулевого смещения:

0,8°/ч

Смещение акселерометра:

00,06 мг

Интерфейс:

СПИ/МОЖЕТ

веса:

50 г

Потребляемая мощность:

1,5 Вт

Название продукта:

ИМУ-гиротехника для БПЛА

Размеры:

47×44×14 мм

Упаковывая детали:

губка + коробка

Поставка способности:

500/месяц

Выделить:

10-axis IMU sensor for drones

low noise IMU gyroscope

high stability drone attitude control

Описание продукта

10-Axis IMU Sensor with ±0.8°/h Bias Stability

High-performance inertial measurement unit designed for drone attitude control applications requiring exceptional precision and low noise characteristics.

Product Overview

The 16488HB Inertial Measurement Unit delivers exceptional performance with its three-axis gyroscope and accelerometer. Engineered for precision applications, this unit provides enhanced stability and reliability, making it an ideal replacement for the Adis 16497 in applications demanding high precision and adaptability.

Key Features

Three-axis digital gyroscope: ±2000°/s dynamic measurement range with zero bias stability of 3°/h (GJB, 10S, Z-axis) and 0.8°/h (ALLAN, Z-axis)
Triaxial digital accelerometer: ±200g dynamic measurement range with zero bias stability of 0.4mg (GJB, 10S) and 0.06mg (ALLAN)
Triaxial digital magnetometer: 2.5 gauss dynamic measurement range
Digital barometer: 300mbar to 1100mbar operating range
High reliability: MTBF 20,000 hours
Full temperature range accuracy: Guaranteed performance from -40℃ to +80℃ with built-in temperature calibration and compensation
Vibration resistance: Suitable for operation under strong vibration (6.06G, 20-2000Hz)
Impact resistance: Capable of withstanding large impact conditions (1000G, 0.5ms)

Technical Specifications

Gyroscope Parameters

Parameter	Test Conditions	Typical Value	Max Value	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	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 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 Parameters

Parameter	Test Conditions	Typical Value	Max Value	Unit
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 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

Additional Parameters

Parameter	Test Conditions	Min Value	Typical Value	Max Value	Unit
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
Dynamic measuring range		300		1100	mbar
Zero bias			4.5		mbar
Baud rate	SPI			15	MHz
Baud rate	CAN			1	MHz
Sampling frequency	SPI	2460	2460		Hz
Sampling frequency	CAN		200		Hz
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
Size			474414		mm
Weight			50		g
Operating temperature		-40		70	℃
Storage temperature		-45		75	℃
Vibration	20~2000Hz, 6.06g
Impact	1000g, 0.5ms
MTBF			20000		h
Continuous working time			120		h

Note 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℃
Note ②: Vibration condition is 6.06G, 20Hz~2000Hz

Outline Drawing

Теги:

Датчик гироскопа акселерометра

Гироскоп акселерометра IMU

Акселерометр сгибания кварца

гироскоп оптического волокна

Инерциальная навигационная система

Искатель гироскопа северный

Датчик магнитометра

Датчик гироскопа акселерометра

Гироскоп акселерометра IMU

Акселерометр сгибания кварца

гироскоп оптического волокна

Инерциальная навигационная система

Искатель гироскопа северный

Датчик магнитометра

Подробная информация о продукции

10-Axis IMU Sensor ±0.8°/h Bias Stability Low Noise for Drone Attitude Control

10-Axis IMU Sensor ±0.8°/h Bias Stability Low Noise for Drone Attitude Control

10-axis IMU sensor for drones

low noise IMU gyroscope

high stability drone attitude control

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