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Home Products

IMU Accelerometer Gyro

Low Dift Gyroscope Accelerometer Inertial Measurement Unit IMU

Name: Low Dift Gyroscope Accelerometer Inertial Measurement Unit IMU
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: 16488C
Price: 3,003.00 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	16488C
MOQ:	1
Price:	negotiable
Payment Terms:	L/C,T/T
Supply Ability:	500/Month

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Certification:

Gyro Range:

±450°/s

Gyro Zero Bias Stability:

5 .1°/h

Acc Range:

±18g

Acc Zero Bias Stability:

0.07mg(Allan)

Interface:

1 Channel SPI/UART/CAN

Bandwidth (-3dB):

330Hz

Random Walk:

0.26º/√h

Power Consumption:

0.6W

Packaging Details:

Sponge/Box

Supply Ability:

500/Month

Highlight:

High performance IMU

Inertial Measurement Unit IMU

Gyroscope Accelerometer IMU

Product Description

Low Dift Gyroscope Accelerometer Inertial Measurement Unit IMU

Product Description

The 16488C multi-degree-of-freedom inertial measurement unit is a complete inertial system with a built-in three-axis gyroscope, a three-axis accelerometer, a three-axis magnetometer and a pressure sensor for measuring the three-axis angle of the carrier parameters such as rate, acceleration, three-axis magnetic field, air pressure, etc., output data after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation, etc.) according to the communication protocol through SPI.

Three-axis digital gyroscope:
1. ± 450º/s dynamic measuring range;
2. Zero-bias stability: 5.1 °/h
Triaxial digital accelerometer:
1. ± 18 g dynamic measuring range;
2. Zero-bias stability: 0.07mg (ALLAN);
High reliability: MTBF > 20000h;
Guaranteed accuracy within the full temperature range (-40 ºC ~ 70 ºC): built-in high-performance temperature calibration and compensation algorithm;
Suitable for working under strong vibration conditions;
Interface 1 channel UART, 1 channel SPI, 1 channel CAN

Technical parameters

parameter		Test Conditions	Minimum	Typical	Maximum	unit
Gyro	Dynamic measuring range	Configurable (maximum ± 1000)		±450		º/s
	Zero bias instability	Allan variance, better than		5.1		º/h
	Zero bias stability	1s smooth, rms, better than		30		º/h
	Zero bias over the full temperature range	-40 ºC ~ 85 ºC, 10s smooth, rms		0.03		º/s
	Random walk	1б		0.26		º/√h
	Zero bias repeatability	1б		100		º/h
	Output noise	No filtering, rms		0.135		º/s
	Scale factor repeatability	1б		0.1		%
	Scale factor nonlinearity	FS=450 º/s		0.01		%FS
	Bandwidth (-3dB)			330		Hz
	Cross coupling			0.1		%
Accelerometer	Dynamic measuring range	Configurable (maximum ± 40)		±18		g
	Zero bias stability	Allan variance		0.07		mg
	Zero bias over the full temperature range	-40 ºC ~ 85 ºC, 10s smooth, rms		5		mg
	Random walk	1б		0.029		m/s/√h
	Zero bias repeatability	1б		5		mg
	Output noise	No filtering, rms		1		mg
	Scale factor repeatability	1б		0.1		%
	Scale factor nonlinearity	FS=10g		0.1		%FS
	Bandwidth (-3dB)			330		Hz
	Cross coupling			0.1		%
Magnetometer	Dynamic measuring range			±2.5		gauss
	Sensitivity			0.1		mgauss/LSB
	Nonlinearity			0.5		%FS
Barometer	Pressure range		300		1100	mbar
	Sensitivity			6.1 × 10^-7		mbar/LSB
	Total error			4.5		mbar
	Relative error			2.5		mbar
	Nonlinearity			0.1		%FS
Communication Interface	1 spi	Input clock frequency			15	MHz
Communication Interface
Electrical characteristics	Voltage	DC	2.5	3.3 ± 10%	5	V
	Power consumption			0.6	1	W
	Ripple	P-P			100	mV
	weight			48±2		g
Use environment	Operating temperature	Scalable	-40		85	ºC
	storage temperature		-55		85	ºC
	vibration			10~2000Hz,6.06g
	Shock			5000g,0.1ms

Dimension

Low Dift Gyroscope Accelerometer Inertial Measurement Unit IMU 0

Payment& Shipping

Low Dift Gyroscope Accelerometer Inertial Measurement Unit IMU 1

Low Dift Gyroscope Accelerometer Inertial Measurement Unit IMU 2

Low Dift Gyroscope Accelerometer Inertial Measurement Unit IMU 3

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

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