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Honeywell HG4930 Replacement MEMS Inertial Measurement Unit for Navigation & Stabilization

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Honeywell HG4930 Replacement MEMS Inertial Measurement Unit for Navigation & Stabilization

Name: Honeywell HG4930 Replacement MEMS Inertial Measurement Unit for Navigation amp Stabilization
Brand: Firepower
Price: 2000 USD

Wholesale Honeywell HG4930 Replacement MEMS Inertial Measurement Unit for Navigation & Stabilization from china suppliers

Brand Name : Firepower

Model Number : HG4930C

Place of Origin : China

MOQ : 1

Price : 2000$

Payment Terms : L/C,D/A,D/P,T/T,Western Union

Supply Ability : 500/month

Delivery Time : 1 Week for sample

Packaging Details : BOX+Sponge

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

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Honeywell HG4930 Replacement MEMS Inertial Measurement Unit for Navigation & Stabilization

Product Description

MEMS Inertial Measurement Unit (IMU) integrates a three-axis gyroscope, three-axis accelerometer, temperature sensor, signal processing board, structural components, and supporting software. It is designed to measure the three-axis angular rate, linear acceleration, and inclination angle of a moving carrier.

The unit performs real-time error compensation — including temperature drift correction, installation misalignment compensation, and nonlinear calibration — and outputs the corrected gyroscope and accelerometer data via an RS-422 serial interface, following a predefined 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 Technical 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

Outline Structure

Honeywell HG4930 Replacement MEMS Inertial Measurement Unit for Navigation & Stabilization

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