IMU Accelerometer Gyro MEMS Inertial Measurement 6 AXIS

Browse Categories

Shenzhen Fire Power Control Technology Co., LTD

City: shenzhen

Province/State:guangdong

Country/Region:china

Tel:86-755-23097872

View Contact Details

IMU Accelerometer Gyro MEMS Inertial Measurement 6 AXIS

Brand Name	Firepower
Model Number	GI200-B0-IMU
Certification	CE
Place of Origin	CHINA
Minimum Order Quantity	1
Price	negotiable
Payment Terms	T/T
Supply Ability	1000/month
Delivery Time	1 week
Packaging Details	Box with sponge
Product name	IMU Gyro for UAV
Gyro measure range	500deg/s
Accelerometer measure range	16g
Gyro Zero bias stability	0.8deg/h
Accelerometer Allan variance	0.03mg
Gryo angular random walk	0.15°/√hr
Power consumption	1.5W
Weight	50g

Detailed Product Description

IMU Accelerometer Gyro Inertial Measurement

Product Description

The GI200-BO (AO) -IMU is an inertial measurement unit (IMU) based on micromachining technology (MEMS), with built-in high-performance MEMS gyroscope and MEMS accelerometer, outputting 3 angular velocities and 3 accelerations.

The GI200-A0 (B0) -IMU is available in A0 (low configuration) and B0 (high configuration) versions.

Main Features

Three-axis digital gyroscope:
1. ± 2000º/s dynamic measurement range;
2. A0 bias stability: 6 °/H (GJB, 10s, Z-axis), 9 °/H (GJB, 1s, Z-axis), 1.6 °/H (ALLAN, Z-axis);
3. B0 bias stability: 3 °/H (GJB, 10s, Z-axis), 4.5 °/H (GJB, 1s, Z-axis), 0.8 °/H (ALLAN, Z-axis);
Triaxial digital accelerometer:
1. ± 200g dynamic measuring range;
2. A0 bias stability: 0.4mg (GJB, 10s), 0.6mg (GJB, 1s), 0.06 mg (ALLAN);
3. B0 bias stability: 0.2mg (GJB, 10s), 0.3mg (GJB, 1s), 0.03mg (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

Technical Indicators

Parameter		Test conditions	Minimum value	Typical value	Maximum value	Unit
Gyro	Dynamic measuring range			500	2000	º/s
	Zero bias stability	Allan variance, Z-axis		0.8		º/h
		Allan variance, X and Y axis		1.6		º/h
		10 s average (-40 ℃ ~ + 80 ℃, constant temperature), Z-axis		3		º/h
		1s average (-40 ℃ ~ + 80 ℃, constant temperature), Z-axis		4.5		º/h
		10 s average (-40 ℃ ~ + 80 ℃, constant temperature), X axis and Y axis		6		º/h
		1 s average (-40 ℃ ~ + 80 ℃, constant temperature), X axis and Y axis		9		º/h
	Zero bias	Zero-bias range, Z-axis		±0.07		º/s
		Zero-bias range, X-axis and Y-axis		±0.2		º/s
		Zero bias change over full temperature range, Z-axis①		±0.02		º/s
		Zero bias change over full temperature range, X and Y axis①		±0.06		º/s
		Successive Start Repeatability, Z-axis		0.002		º/s
		Successive Start Repeatability, X-Axis and Y-Axis		0.006		º/s
		Daily start repeatability, Z-axis		0.003		º/s
		Daily start repeatability, X axis and Y axis		0.009		º/s
		Effect of linear acceleration on bias		0.002		º/s/g
		Influence of vibration on zero bias, change before and after vibration②		0.002		º/s/g
		Influence of vibration on zero bias, change before and during vibration②		0.002		º/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		º/s/LSB
	Bandwidth			200		Hz
Accelerometer	Dynamic measuring range			16	200	g
	Zero bias stability	Allan variance		0.03		mg
		10 s average (-40 ℃ ~ + 80 ℃, constant temperature)		0.2		mg
		1s average (-40 ℃ ~ + 80 ℃, constant temperature)		0.3		mg
	Zero bias	Zero bias range		5		mg
		Zero bias change in full temperature range, peak-to-peak value①		5		mg
		Repeatability of successive starts		0.5		mg
		Daily start repeatability		0.8		mg
		Zero-bias temperature coefficient		0.05	0.1	mg/℃
	Scale factor	Scale factor accuracy		0.5		%
	Scale factor	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	B_rg,xy		±1300		μT
	Magnetic field range	B_rg,z		±2500		μT
	Resolution			0.3		μT
	Heading and longitude	30 μT horizontal geomagnetic component, 25 ℃		±2.5		deg
Communication interface	1-channel SPI	Baud rate			15	MHz
	1-channel UART	Baud rate		230.4		Kbps
	1-channel CAN	Baud rate			1	MHz
	Sampling frequency	SPI		200	1000	Hz
		UART		200		Hz
		CAN		200
Electrical characteristics	Voltage		3	3.3	3.6	V
	Power consumption				1.5	W
	Ripple	P-P			100	mV
Structural characteristics	Size			47×44×14		mm
Structural characteristics	Weight			50		g
Use environment	Operating temperature		-40		80	℃
	Storage temperature		-45		85	℃
	Vibration			20~2000Hz,6.06g
	Impact			1000g,0.5ms
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 ℃ ~ + 80 ℃;
2: Vibration condition is 6.06 G, 20Hz ~ 2000Hz

Electrical Interface

Product Dimension

L47mm x W44mm x H14mm(L x W x H)

Product Tags: Cutting-Edge IMU Accelerometer Gyro UAV IMU Accelerometer Gyro IMU Accelerometer Gyro for UAV

Related Products

Lightweight 6-axis Inertial Measurement Unit Accelerometer Gyroscope Sensor

IMU Accelerometer Gyro With High Environmental Adaptability

Compact and Low Weight IMU Inertial Sensor Inertial Measurement Unit

Stim300 IMU Accelerometer Gyro Sensor Factory Supply

Temperature Compensated IMU Accelerometer Gyro 16488-C 3 axis

6 Axis IMU Accelerometer Gyro Inertial Measure Unit Low Cost

Email to this supplier


From:	Enter your Email please. Your email is incorrect!
To:	Shenzhen Fire Power Control Technology Co., LTD
Subject:	Subject is empty!
Message:	Characters Remaining: (80/3000) Please enter 20 to 3000 characters to contact this supplier!