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Inertial Measurement Unit IMU 6-Axis Accelerometer Gyroscope

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

Gyro Range:

±200°/s

Gyro Bias Instability:

<0.2º/h

Bandwidth:

≤100Hz

Random Walk:

0.02°/√h

Acc Range:

±30g

Zero-bias Stability (Allan Variance @ 25 ℃):

30ug

Zero-bias Repeatability:

2mg

Vibration:

10~2000Hz，6.06g

Packaging Details:

carton with sponge

Supply Ability:

1000pcs

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Product Description

Inertial Measurement Unit IMU 6-Axis Accelerometer Gyroscope

MEMS Inertial Measurement Unit (IMU) integrates a three-axis gyroscope, three-axis accelerometer, temperature sensor, signal processing board, and necessary software in a compact, robust package. It accurately measures 3-axis angular rate, acceleration, and inclination of a carrier and outputs error-compensated data (temperature, misalignment, nonlinear corrections) via RS-422. Designed for navigation, attitude control, and stabilization, this IMU is a reliable replacement for Honeywell HG4930, suitable for UAVs, autonomous vehicles, and aerospace platforms.

Main 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

Other Specifications

Parameter	Unit	HG4930C
Weight	g	120

Outline Drawing

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

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