Honeywell

HG9900 Inertial Measurement Unit

HG9900 Inertial Measurement Unit — inertial measurement units from Honeywell

The HG9900 is a high performance navigation-grade Inertial Measurement Unit (IMU) designed to meet the needs of a broad range of navigation, guidance and control applications. The HG9900 has been successfully deployed on a wide range of weaponry, UAVs, stabilized platforms and commercial applications. The HG9900's three Ring Laser Gyroscopes (RLGs), three Quartz Accelerometers (QAs) and associated electronics are all environmentally sealed in rugged aluminum housing. In addition, it employs an internal environmental isolator system to filter unwanted sensor inputs commonly encountered in real world applications. Honeywell designs, develops and manufactures all of the inertial sensors utilized in the HG9900 IMU. All of this culminates in the HG9900 providing industry leading inertial sensor performance while maintaining minimal SWAP parameters. The HG9900 is designed and built at a Honeywell facility in the USA. It typically has an ECCN of 7A003.d but can vary depending on model selected. It generally requires an export license

The HG9900's three Ring Laser Gyroscopes (RLGs), three Quartz Accelerometers (QAs) and associated electronics are all environmentally sealed in rugged aluminum housing. In addition, it employs an internal environmental isolator system to filter unwanted sensor inputs commonly encountered in real world applications. Honeywell designs, develops and manufactures all of the inertial sensors utilized in the HG9900 IMU. All of this culminates in the HG9900 providing industry leading inertial sensor performance while maintaining minimal SWAP parameters.

The HG9900 is designed and built at a Honeywell facility in the USA. It typically has an ECCN of 7A003.d but can vary depending on model selected. It generally requires an export license

Specifications

Performance: Accelerometer Sensor TechnologyQuartz
Performance: Accel Bias Repeatability (mg 1σ)0.0025
Performance: Accel Bias In-Run Stability (mg 1σ)0.025
Performance: Gyro sensor technologyRing Laser
Performance: Gyro Operating Range-40°/s to +71°/s
Performance: Gyro ARW0.0021
Performance: Gyro Bias In-Run Stability0.0021 °∕hr 1σ
Performance: Gyro Bias Repeatability0.0021 °∕hr 1σ
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