Home > IMU Accelerometer Gyro >

MEMS Based Inertial Measurement Unit With High Performance

Product Categories

Shenzhen Fire Power Control Technology Co., LTD

Trust Seal

Verified Supplier

Credit Check

Supplier Assessment

Contact Now

MEMS Based Inertial Measurement Unit With High Performance

Name: MEMS Based Inertial Measurement Unit With High Performance
Brand: Firepower
Price: 1 USD

Brand Name : Firepower

Model Number : 16497

Certification : CE ROHS

Place of Origin : CHINA

MOQ : 1

Price : negotiable

Payment Terms : T/T, L/C

Supply Ability : 500/month

Packaging Details : sponge/box

Product name : MEMS Inertial Measurement Unit

Measuring range : ±500º/s

zero bias stability : 1deg/h

Zero-bias repeatability : 0.1deg/s

cale factor nonlinearity : 0.02%F

accelerometer range : 16g

Zero bias stability : 0.5mg

Contact Now

MEMS Based Inertial Measurement Unit With A High-Performance MEMS Gyroscope And Accelerometer

1. Product overview

The 16497C-C0-IMU is a micromachining technology (MEMS) based inertial measurement unit (IMU) with a high-performance MEMS gyroscope and MEMS

The accelerometer outputs 3 angular velocities and 3 accelerations.

The 16497C-C0-IMU features high reliability and strong environmental adaptability. By matching different software, the product can be widely used in intelligent driving, tactical and industrial UAV, intelligent ammunition, seeker, mobile communication, mapping, stable platform and other fields.

2. Product features

Three-axis digital gyroscope:
1. ± 500º/s dynamic measuring range;
2. Zero bias stability: 5 °/H (GJB, 10s), 1.0 °/H (ALLAN);
Triaxial digital accelerometer:
1. ± 16 G dynamic measuring range;
2. Zero-bias stability: 0.5mg (GJB, 10s), 0.1mg (ALLAN);
High reliability: MTBF > 20000h;
Guaranteed accuracy within the full temperature range (-40 ℃ ~ 80 ℃): 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

3. Field of application

Intelligent driving
Tactical and Industrial UAV
Smart Munitions
Seeker
Communication in motion
Mapping
Stabilize the platform

4. Product indicators

Parameter		Test conditions	Minimum value Typical value	Maximum value	Unit
	Dynamic measuring range			500	º/s
	Zero bias stability	Allan variance 10 s average (-40 ℃ ~ + 80 ℃, constant temperature)	1.0 5		º/h º/h
Peg-top	Zero bias	Zero-bias range Zero bias change over full temperature range ○ 1	±0.2 ±0.06		º/s º/s
	Scale factor	Scale factor accuracy Scale factor nonlinearity	0.3 0.02		% %FS
	Resolution		3.052×10⁻7		º/s/LSB
	Bandwidth		200		Hz
	Dynamic measuring range		16		g mg mg mg mg % %FS g/LSB Hz
	Zero bias stability	Allan variance 10 s average (-40 ℃ ~ + 80 ℃, constant temperature)	0.1 0.5
Accelerometer	Zero bias	Zero-bias range Change of zero bias within full temperature range, peak-to-peak value ○ 1	2 2
	Scale factor	Scale factor accuracy Scale factor nonlinearity	0.3 0.02
	Resolution		1.221×10⁻8
	Bandwidth		200
Communication interface	1-way SPI	Baud rate	15		MHz

Parameter		Test conditions	Minimum value	Typical value	Maximum value	Unit
1-way UART		Baud rate		230.4		Kbps
1-way CAN		Baud rate			1	MHz
		SPI		200	1000	Hz
Sampling frequency		UART		200		Hz
		CAN		200		Hz
	Voltage		3.0	3.3	3.6	V
Electrical characteristics	Power consumption				1.5	W
	Ripple	P-P			100	mV
Structural characteristics	Size		47×44×14			mm
	Weight		50			g
Use environment	Operating Temperature Storage Temperature Vibration Impact		-40		80	℃
			-45		85	℃
				20~2000Hz,
				6.06g
				1000g,0.5ms
Reliability	MTBF		20000			h
	Continuous working time		120			h

IMU polarity definition

3 gyros and 3 accelerometers is defined as shown in the figure below, and the direction of the arrow is positive.

Product Tags: