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Honeywell Aerospace HG4930 MEMS Inertial Measurement Unit

High Performance MEMS IMU

The HG4930 is a very high performance Micro-Electro-Mechanical System (MEMS) based Inertial Measurement Unit (IMU) designed to meet the needs of applications across various markets including agriculture, AUVs, industrial equipment, robotics, survey/mapping, stabilized platforms, transportation, UAVs, and UGVs.

  • Honeywell Aerospace HG4930 MEMS Inertial Measurement Unit
Honeywell Aerospace
2600 Ridgway Pkwy
MN 55413 Minneapolis
United States
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Description

The HG4930 is a very high performance Micro-Electro-Mechanical System (MEMS) based Inertial Measurement Unit (IMU) designed to meet the needs of applications across various markets including agriculture, AUVs, industrial equipment, robotics, survey/mapping, stabilized platforms, transportation, UAVs, and UGVs. With industry standard communication interfaces the HG4930 is easily integrated into a variety of architectures. The extremely small size, light weight and low power make the HG4930 ideal for most applications.

The HG4930 includes MEMS gyroscopes and accelerometers. In addition, the HG4930 employs an internal environmental isolation system to attenuate unwanted inputs commonly encountered in real world applications. The internal isolation and other proprietary design features ensure the HG4930 is rugged enough to meet the needs of the most demanding users.

The HG4930 is not ITAR controlled. Its Export Control Classification Number (ECCN) is 7A994.

Visit https://aerospace.honeywell.com/en/products/navigation-and-sensors/hg4930 for more information.

Specifications

  • System components
    Accelerometer(s), Gyroscope(s)
  • Height [mm]
    65
  • Width [mm]
    51
  • Length [mm]
    35.5
  • Weight [gr]
    140
  • Min. Voltage (DC)
    4.75
  • Max. Voltage (DC)
    5.25
  • Power consumption [W]
    2
  • Min. operating temperature [C]
    -54
  • Max. operating temperature [C]
    85
  • Interface types
    Digital
  • Interfaces
    RS-422
  • Other interfaces and additional information
    Fully Compensated Incremental/Delta Outputs are Ready for Integration into Position/Attitude. Stabilization Configurations Optimize Latency & Bandwidth Without Sacrificing Accuracy.
  • Max. rotation speed [deg/s]
    200
  • Range [± ° / sec]
    200
  • In-Run Bias Stability [ °/ hr]
    0.25
  • Distinguishable features
    The internal isolation and other proprietary design features ensure the HG4930 is rugged enough to meet the needs of the most demanding users.
  • Application
    Whether the platform is autonomous or manned and operates in the land, sky, or sea the HG4930 is designed to meet the needs of a range of industries including: Agriculture, Automotive, Communication, Construction, Energy, Inspection, Mapping, Marine (Surface & Subsea), Mining, Robotics, Surveillance, and Transportation.
  • Range [max g]
    20
  • In-Run Bias Stability [mg]
    0.025

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