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Advanced MEMS Inertial Measurement Unit Sensor with 0.2° Bias Honeywell HG4930C IMU

Name: Advanced MEMS Inertial Measurement Unit Sensor with 0.2° Bias Honeywell HG4930C IMU
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: HG4930C
Price: 2000 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	HG4930C
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:

±200°/s

Zero-bias Stability (@ Allan Variance):

0.2°/h

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

0.5°/h

Random Walk:

0.02°/√h

Scale Factor Repeatability (1σ ):

1°/h

3 DB Bandwidth:

100Hz

Accelerometer Bias Stability:

30ug

Acc Measuring Range (customizable):

30g

Weight:

120g

Power Consumption:

1.5W

Packaging Details:

BOX+Sponge

Supply Ability:

500/month

Highlight:

Honeywell Inertial Measurement Unit

Advanced MEMS Inertial Measurement Unit

0.2° Bias Inertial Measurement Unit

Product Description

Advanced MEMS Inertial Measurement Unit Sensor with 0.2° Bias Honeywell HG4930C IMU

Key Specifications

Attribute	Value
Gyro Measuring range	±200°/s
Zero-bias stability (@ Allan variance)	0.2°/h
Zero-bias stability (10 s smoothing, 1σ, room temperature)	0.5°/h
Random walk	0.02°/√h
Scale Factor Repeatability (1σ)	1°/h
3 dB Bandwidth	100Hz
Accelerometer bias stability	30ug
Acc Measuring range (customizable)	30g
Weight	120g
Power consumption	1.5W

Product Overview

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

Technical Specifications

Gyroscope Performance

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 Performance

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 Specifications

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

Outline Structure

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

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