Home > IMU Accelerometer Gyro >

Built In MEMS Gyroscope IMU Inertial Measurement Unit Based On MEMS

Product Categories

Shenzhen Fire Power Control Technology Co., LTD

Trust Seal

Verified Supplier

Credit Check

Supplier Assessment

Contact Now

Built In MEMS Gyroscope IMU Inertial Measurement Unit Based On MEMS

Name: Built In MEMS Gyroscope IMU Inertial Measurement Unit Based On MEMS
Brand: Firepower
Price: 1 USD

Brand Name : Firepower

Model Number : IMU200B

Certification : CE ROHS

Place of Origin : China

MOQ : 1

Payment Terms : T/T

Supply Ability : 200/month

Packaging Details : sponge/box

Gyro bias stability : 8°/h

gyro Repeatability : 15°/h

Daily start repeatability : 30°/h

Zero bias : 0.15°/s

accelerometer bias : 5mg

accelerometer scale factor : 3000 ppm

Power supply : 5±0.1 v

Contact Now

Inertial Measurement Unit (IMU) Based On Micromachining Technology (MEMS) With Built-In High-Performance MEMS Gyroscope

The IMU200B-IMU is an inertial measurement unit (IMU) based on micromachining technology (MEMS) with built-in high-performance MEMS gyroscope and MEMS accelerometer, which outputs 3 angular velocities and 3 accelerations.

The IMU200B-IMU features high reliability and strong environmental adaptability. By matching different software, the product can be widely used in tactical and industrial UAV, smart ammunition, seeker and other fields.

Product features

Three-axis digital gyroscope:
1. ± 500º/s dynamic measuring range;
2. Zero bias stability: 8 °/H (GJB, 10s), 1.9 °/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-way RS422

			Test conditions	Typical value
Angular velocity
	Zero bias	Stability	10 s average, + 70 ℃, + 20 ℃, -40 ℃
		Stability	Allan variance, + 20 ℃		2.85	3.8
		Repeatability of successive starts	℃,+20℃,-40℃		22.5	30
		Daily start repeatability	℃,+20℃,-40℃		45	60
		Monthly Start Repeatability	℃,+20℃,-40℃		90	120
		Zero-bias total temperature variation	-40 ℃ ~ + 70 ℃, 1 ℃/min, 10 s average, 1σ		0.03	0.04
		Zero bias	Life-cycle change, accelerated testing		0.225	0.3
	Scale factor	Repeatability of successive starts	℃,+20℃,-40℃		150	200
		Daily start repeatability	℃,+20℃,-40℃		300	400
		Monthly Start Repeatability	℃,+20℃,-40℃		600	800
		Non-linearity	℃		300	400
		Full temperature change	℃/min,1σ		600	800
		Scale factor	Life-cycle change, accelerated testing		4500	6000
	Acceleration sensitive term
	Random walk						°/√hr
	Noise density						°/s/√Hz
	Bandwidth
	Data delay		Excluding transmission time

	Zero bias	Stability	10 s average, + 70 ℃, + 20 ℃, -40 ℃
		Stability	Allan variance, + 20 ℃
		Repeatability of successive starts	℃,+20℃,-40℃
		Daily start repeatability	℃,+20℃,-40℃
		Monthly Start Repeatability	℃,+20℃,-40℃
		Zero-bias total temperature variation	-40 ℃ ~ + 70 ℃, 1 ℃/min variation
		Zero bias	Life-cycle change, accelerated test instead
	Scale factor	Repeatability of successive starts	℃,+20℃,-40℃
		Daily start repeatability	℃,+20℃,-40℃
		Monthly Start Repeatability	℃,+20℃,-40℃
		Non-linearity	℃
		Full temperature change	After full temperature calibration and compensation, 1 ℃/min, 10 s average peak-peak value
		Scale factor	Life-cycle change, accelerated test instead
	Bandwidth
	Data delay		Excluding transmission time
Start time			Time from power up to output valid data
Reset time			Time from reset to output valid data (hard reset)
Reset time			Time from reset to output valid data (soft reset)
3 gyro axes and 3 acceleration axes The degree of nonorthogonality between any two ax			℃,+20℃,-40℃
Power supply
Power consumption
Communication update rate			1-way RS422	200 (default) 500 (Max)
Communication baud rate			1-way RS422	230.4 (default) 921.6 (Max)

Product Tags: