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Honeywell HG4930 Replacement MEMS Inertial Measurement Unit for Navigation & Stabilization

Honeywell HG4930 Replacement MEMS Inertial Measurement Unit for Navigation & Stabilization

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
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:

Navigation Inertial Measurement Unit

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Stabilization Inertial Measurement Unit

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Honeywell Inertial Measurement Unit

Product Description
Honeywell HG4930 Replacement MEMS Inertial Measurement Unit for Navigation & Stabilization
Product Attributes
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 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 0