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Adis16488 Inertial Sensor IMU for UAV and Drone Stabilization System with Magnetometer

Name: Adis16488 Inertial Sensor IMU for UAV and Drone Stabilization System with Magnetometer
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: 16488HB
Price: 3,003.00 USD
Availability: InStock

Nome da marca:	FIREPOWER
Número do modelo:	16488HB
MOQ:	1
Condições de pagamento:	L/C,T/T
Capacidade de abastecimento:	500/mês

Informações pormenorizadas

Descrição do produto

Informações pormenorizadas

Lugar de origem:

China

Faixa de medição dinâmica:

± 2000º/s

estabilidade de viés zero:

3 °/h

Caminhada aleatória angular:

0,15 °/ √h

Precisão do fator de escala, eixo Z:

0,3%

Largura de banda:

200Hz

Interface de comunicação:

SPI/CAN

Detalhes da embalagem:

esponja + caixa

Habilidade da fonte:

500/mês

Destacar:

Adis16488 IMU with magnetometer

UAV stabilization IMU sensor

drone gyro accelerometer system

Descrição do produto

ADIS16488 Inertial Sensor IMU for UAV and Drone Stabilization System with Magnetometer

The ADIS16488HB multi-degree-of-freedom inertial measurement unit is a complete inertial system featuring a three-axis gyroscope, three-axis accelerometer, three-axis magnetometer, and pressure sensor. This advanced IMU measures three-axis angular rate, acceleration, three-axis magnetic field, air pressure, and other critical parameters. The unit outputs error-compensated data (including temperature compensation, installation misalignment angle compensation, and nonlinear compensation) through SPI or UART communication protocols.

Technical 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
		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/℃
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			474414		mm
Structural characteristics	Weight			50		g
Use environment	Operating temperature		-40		70	℃
Use environment	Storage temperature		-45		75	℃
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

Table 1. 16488HB Product Index

Outline Drawing

Tags:

Sensor do giroscópio do acelerômetro

Giroscópio do acelerômetro de IMU

Acelerômetro do flexure de quartzo

giroscópio da fibra ótica

Sistema de navegação com inércia

Inventor norte do giroscópio

Sensor do magnetômetro

Sensor do giroscópio do acelerômetro

Giroscópio do acelerômetro de IMU

Acelerômetro do flexure de quartzo

giroscópio da fibra ótica

Sistema de navegação com inércia

Inventor norte do giroscópio

Sensor do magnetômetro

Detalhes dos produtos

Adis16488 Inertial Sensor IMU for UAV and Drone Stabilization System with Magnetometer

Adis16488 Inertial Sensor IMU for UAV and Drone Stabilization System with Magnetometer

Adis16488 IMU with magnetometer

UAV stabilization IMU sensor

drone gyro accelerometer system

Giroscópio do acelerômetro de ADIS16488 IMU

Unidade de medida com inércia da NÉVOA IMU

Unidade de medida com inércia pequena de MEMS

Fornecimento de fábrica de sensores giroscópicos do acelerômetro Stim300 IMU

Unidade de medição inercial de 6 eixos acelerômetro sensor giroscópio leve

Linha central compensada temperatura do giroscópio 16488-C 3 do acelerômetro de IMU

Unidade de medição de inércia com sensor de inércia da IMU compacta e de baixo peso

Giro acelerômetro IMU com elevada adaptabilidade ao ambiente