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Honeywell HG4930 High-Precision Inertial Measurement Unit IMU for Navigation

Brand Name:	Firepower
Model Number:	HG4930C
MOQ:	1
Payment Terms:	T/T,L/C
Supply Ability:	1000pcs

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Angular Random Walk:

0.02°/√h

Gyro Bias Stability:

0.2°/h

Acc Bias Stability:

30ug

Zero-bias Stability (10 S Smoothing, 1σ, Room Temperature):

0.5°/h

Resolution:

2°/h

Scale Factor Repeatability:

100ppm

Packaging Details:

carton with sponge

Supply Ability:

1000pcs

Highlight:

Vertical Vibration Table Testing

Calibrate Vibration Table Testing

Acceleration Simulating vibration table for testing

Product Description

Honeywell HG4930 High-Precision Inertial Measurement Unit IMU for Navigation

The MEMS Inertial Measurement Unit (IMU) integrates a three-axis gyroscope, three-axis accelerometer, temperature sensor, signal processing board, and supporting software. This precision instrument measures three-axis angular rate, three-axis acceleration, and three-axis inclination angle of a carrier. It outputs compensated gyroscope and accelerometer data (including temperature compensation, installation misalignment angle compensation, and nonlinear compensation) via RS-422 serial port using a standardized communication protocol.

Technical Specifications

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

Physical Specifications

Parameter	Unit	HG4930C
Weight	g	120

Product Diagram

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

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

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

products details

Honeywell HG4930 High-Precision Inertial Measurement Unit IMU for Navigation

Honeywell HG4930 High-Precision Inertial Measurement Unit IMU for Navigation

Vertical Vibration Table Testing

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Acceleration Simulating vibration table for testing

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