products details

Home Products

Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output

Brand Name:	Firepower
Model Number:	IMU6-1
MOQ:	1
Price:	2000$
Payment Terms:	L/C,D/A,D/P,T/T,Western Union
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

China

Gyro Measuring Range:

±400°/s

Bias Stability:

0.3°/h

Angular Random Walk:

0.15º/√h

Bias Repeatability (1σ ):

1°/h

Scale Factor Repeatability (1σ ):

150ppm

3 DB Bandwidth:

250Hz

Accelerometer Bias Stability:

0.02mg

Weight:

55g

Misalignment:

±0.05°

Power Consumption:

Packaging Details:

BOX+Sponge

Supply Ability:

500/month

Highlight:

Aerospace Defense Inertial Measurement Unit

Strong Shock Inertial Measurement Unit

RS-422 Inertial Measurement Unit

Product Description

Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output

Product Description

IMU6 MEMS Inertial Measurement Unit is a highly integrated sensing system that combines a three-axis gyroscope, three-axis accelerometer, three-axis inclinaion angle, temperature sensor, signal processing board, mechanical housing, and accompanying software.

It is designed to measure the three-axis angular rate, three-axis linear acceleration, and three-axis inclination angle of a moving platform or carrier. The system performs comprehensive error compensation, including:

Temperature compensation
Installation misalignment correction
Nonlinear compensation, among others

After compensation, the sensor outputs high-accuracy gyroscope, accelerometer, and inclination data via a standard RS-422 serial interface, following a predefined communication protocol.

The IMU6 is suitable for applications that require compact, robust, and precise inertial sensing in challenging environments.

Technical Parameters

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

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

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

Electrical Characteristics

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

Environmental Adaptability

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

Weight

55±5

Outline Structure

Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output 0

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

products details

Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output

Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output

Aerospace Defense Inertial Measurement Unit

Strong Shock Inertial Measurement Unit

RS-422 Inertial Measurement Unit

Tilt Angle Specification (not Configured by Default, Optional)

Environmental Adaptability