Advanced Inertial Measurement Unit (IMU) Hypersonic Flight Test Results

In late 2024, we successfully conducted the first ever hypersonic flight testing of the Advanced Inertial Measurement Unit (IMU). This technology is in development by Northrop Grumman (NGC), in partnership with the U.S. Army Combat Capabilities Development Command (DEVCOM) Aviation & Missile Center (AvMC) and NTA Inc. for demanding GPS denied applications. The next generation IMU is based on in-house milliHemispherical Resonator Gyroscope (mHRG) and Silicon Accelerometer (SiAc) sensors. The sensor technologies are integrated with modern electronics and firmware in a selfcontained and rugged unit with cutting edge Size, Weight, and Power (SWAP). The main purpose of the completed round of flight testing was to objectively validate a technology maturity milestone for the new IMU in representatively extreme flight regimes and environments using a reusable hypersonic vehicle.

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Published
2025-05-04
DOI
https://doi.org/10.1109/inertial63280.2025.11037214
Primary Topic
Space Exploration and Technology
Type
article
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article

Advanced Inertial Measurement Unit (IMU) Hypersonic Flight Test Results

Alexander A. Trusov, Stephen Pethel, P. G. Renfroe, Aaron Hofmann et al.
Space Exploration and Technology
article

Advanced Inertial Measurement Unit (IMU) Hypersonic Flight Test Results

Alexander A. Trusov, Stephen Pethel, P. G. Renfroe, Aaron Hofmann, Michael A. Chavez, Young Ah Choi, P. S. Clark, Jorge A. Gutiérrez, David Scott, Cole Umemura, Brian Irelan, Farzin Dinyarian, Daniel Rampacek, Simon Berman, Lawrence Linick
article en

Abstract

In late 2024, we successfully conducted the first ever hypersonic flight testing of the Advanced Inertial Measurement Unit (IMU). This technology is in development by Northrop Grumman (NGC), in partnership with the U.S. Army Combat Capabilities Development Command (DEVCOM) Aviation & Missile Center (AvMC) and NTA Inc. for demanding GPS denied applications. The next generation IMU is based on in-house milliHemispherical Resonator Gyroscope (mHRG) and Silicon Accelerometer (SiAc) sensors. The sensor technologies are integrated with modern electronics and firmware in a selfcontained and rugged unit with cutting edge Size, Weight, and Power (SWAP). The main purpose of the completed round of flight testing was to objectively validate a technology maturity milestone for the new IMU in representatively extreme flight regimes and environments using a reusable hypersonic vehicle.

United States Army Combat Capabilities Development Command (US), Northrop Grumman (United States) (US), U.S. Army Combat Capabilities Development Command Aviation & Missile Center, U.S. Army Space and Missile Defense Command (US)
Affordable and clean energy
Openalex Percentile: Top 81%
Space Exploration and Technology
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Advanced Inertial Measurement Unit (IMU) Hypersonic Flight Test Results — Alexander A. Trusov, Stephen Pethel, et al. · (2025) | TGRS Research Map | TGRS