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Low-Noise MEMS IMU for Drone Manufacturer

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Low-Noise MEMS IMU for Drone Manufacturer

Name: LowNoise MEMS IMU for Drone Manufacturer
Brand: Firepower
Price: 1 USD

Buy cheap Low-Noise MEMS IMU for Drone Manufacturer product

Brand Name : Firepower

Model Number : IMU6-1A

Place of Origin : China

MOQ : 1

Payment Terms : T/T,L/C

Supply Ability : 1000pcs

Delivery Time : 1 week

Packaging Details : wooden carton

In-Run Bias Stability(@ Allan variance) : 0.1°/h

Gyro Range : ±400º/s

Angular Random Walk : 0.15 °/√h

Accelerometer Range : ±30

Accelerometer Bias Stability : 0.05mg

3 dB Bandwidth : 200Hz

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1.1 Main Technical Parameters

1.1.1 Gyroscope Specifications

Parameter	Unit	IMU6-1	IMU6-1A	IMU6-1B	IMU6-1C
Measuring range (customizable)	°/s	±400	±400	±400	±2000
In-Run Bias Stability(@ Allan variance)	°/h	0.3	0.1	0. 05	1
Bias stability @10s (10s smooth, 1σ, room temperature)	°/h	3	1	0.5	6
Bias stability in full temperature	°/h	10	3	2	18
Angular Random Walk	°/√h	0.15	0.1	0.02	0.3
Bias repeatability (1σ )	°/h	1	0.5	0.3	2
Bias acceleration sensitivity	°/h/g	1	1	1	2
Scale Factor Non-Linearity(1σ )	ppm	150	150	150	300
Scale Factor Repeatability (1σ )	ppm	20	20	20	100
Misalignment	°	±0.05	±0.05	±0.05	±0.05
3 dB Bandwidth	Hz	250	200	150	250

1.1.2 Accelerometer Technical Indicators

Parameter	Unit	IMU6-1y-1	IMU6-1y-2		IMU6-1y-3		IMU6-1y-4
Measuring range (customizable)	g	±10	±30		±50		±80
In-Run Bias Stability (Allan Variance @ 25 ℃)	mg	0.02	0.05		0.1		0.2
Bias stability @10s	mg	0.05	0.2		0.5		1
Bias stability in full temperature	mg	1	3		5		15
Angular Random Walk	m/s/√h	0.001	0.002		0.005		0.01
Bias repeatability(1σ )	mg	0.1	0.5		1		2
Scale Factor Repeatability (1σ )	ppm	200	200			200		200
Scale Factor Non-Linearity(1σ )	ppm	50		100		200		300
Misalignment	°	±0.05		±0.05		±0.05		±0.05
3 dB Bandwidth	Hz	100		100		100		100

1.1.3 Tilt Angle Specification (not Configured by Default, Optional)

Parameter	Unit	IMU6-1y-x
Measuring range (customizable)	g	±1.7
Bias stability (1s smoothing)	mg	0.5
Random walk	m/s/√h	0.08
Scale factor non-linearity	ppm	100

1.1.4 Electrical Characteristics

Parameter	Unit	IMU6-1y-x
Voltage	V	5
Power consumption	W	2
Ripple	mV	100

1.1.5 Environmental Adaptability

Parameter	Unit	IMU6-1y-x
Operating temperature	℃	-45~85
Storage temperature	℃	-55~105
Vibration	--	10~2000Hz,6.06g
Impact	--	1000g,0.1ms

1.1.6 Other

Parameter	Unit	IMU6-1y-x
Weight	g	55±5

MEMS IMU is a fully integrated system combining gyroscope, accelerometer, inclinometer, temperature sensor, and processing electronics. It provides real-time 3-axis angular rate, acceleration, and inclination measurements with error compensation. Compact and lightweight, it outputs data through RS-422 for easy integration. Suitable for aerospace, defense, and autonomous vehicle navigation, this IMU serves as a direct replacement for STIM300, delivering reliable, stable performance under harsh conditions.

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