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Tactical-Grade Inertial Measurement Unit Sensor Hg4930 Honeywell Replacement

Brand Name:	FIREPOWER
Model Number:	HG4930C
MOQ:	1
Price:	3500$
Payment Terms:	L/C,T/T,Western Union
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

China

Gyroscope Range:

±200°/s

Gyroscope Zero-Bias Instability:

0.2°/h

Zero-Bias Repeatability:

1°/h

Random Walk:

0.02°/√h

Accelerometer Range:

±30g

Accelerometer Zero-Bias Stability:

30ug

Scale Factor Nonlinearity:

500ppm

Bandwidth (-3dB):

100Hz

Packaging Details:

sponge+box

Supply Ability:

500/month

Highlight:

Hg4930 Inertial Measurement Unit Sensor

Tactical-Grade Inertial Measurement Unit Sensor

Honeywell Replacement Inertial Measurement Unit Sensor

Product Description

Product Description

The MEMS Inertial Measurement Unit (IMU) consists of three-axis gyroscope, three-axis accelerometer, temperature sensor, signal processing board, structure and necessary software, and is used for measuring the three-axis angular rate, three-axis acceleration and three-axis inclination angle of a carrier. And output the data of the gyroscope and the accelerometer after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation and etc) through RS-422 serial port according to an agreed communication protocol.

Technical Parameters

Gyroscope specifications

Parameter	Unit	HG4930C
Measuring range (customizable)	°/s	±200
Zero-bias stability (@ Allan variance)	°/h	0.2
Zero-bias stability (10 s smoothing, 1σ, room temperature)	°/h	0.5
Zero-bias error over full temperature range	°/h	2.5
Random walk	°/√h	0.02
Zero-bias repeatability	°/h	1
Zero bias acceleration sensitivity	°/h/g	1
Resolution	°/h	2
Scale factor nonlinearity	ppm	100
Scale factor repeatability	ppm	100
Cross coupling	%	0.2
Bandwidth	Hz	100

Accelerometer indicators

Parameter	Unit	HG4930C

Measuring range (customizable)	g	±30
Zero-bias stability (Allan Variance @ 25 ℃)	ug	30
Zero-bias stability (1s smoothing)	ug	700
Zero-bias error over full temperature range	mg	1.5
Random walk	m/s/√h	0.01
Zero-bias repeatability	mg	2
Scale factor repeatability	ppm	200
Scale factor nonlinearity	ppm	200
Cross coupling	%	0.2
Bandwidth	Hz	100

Electrical characteristics

Parameter	Unit	HG4930C
Voltage	V	5
Power consumption	W	1.5
Ripple	mV	100

Environmental adaptability

Parameter	Unit	HG4930C
Operating temperature	℃	-45~85
Storage temperature	℃	-60~105
Vibration	--	10~2000Hz,6.06g
Impact	--	15000g,4ms

Weight

120

Outline Drawing

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

Tactical-Grade Inertial Measurement Unit Sensor Hg4930 Honeywell Replacement

Tactical-Grade Inertial Measurement Unit Sensor Hg4930 Honeywell Replacement

Hg4930 Inertial Measurement Unit Sensor

Tactical-Grade Inertial Measurement Unit Sensor

Honeywell Replacement Inertial Measurement Unit Sensor

Gyroscope specifications

Accelerometer indicators

Electrical characteristics

Environmental adaptability