SBIR/STTR Research Award

Real Time Models for Predicting Optical Seeker Window Distortions for HWIL

Award identifier 5a668f807d6ba708b1b0d840a568cf2ecb4d8cc9ccdde69ee0c528e8df8d6a4dAwarding agency Department of Defense · Air Force

Award amount

$139,879

Program and phase

SBIR · Phase I

Award year

2025

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
CFD Research Corporation
Proposal award date
2025-04-23
Contract end date
2025-10-18
UEI
V3KCP1HNFM33
Solicitation number
24.4
Topic code
AF244-0005

Research abstract

Hypersonic vehicles are designed to pursue deeply protected targets at very high speeds and long ranges, making them a critical offensive and defensive technology. As such, the U.S. Air Force, U.S. Navy and other DoD agencies have identified a growing need to develop hypersonic missile systems. New technologies have been pushing the system limits of speed, range, and high-temperature exposure times. These extreme conditions make designing many of the critical components of a hypersonic vehicle very challenging. Reproducing the operating conditions in ground test facilities is nearly impossible, while test flights can be cost prohibitive especially during early design phases. Tests for avionic software can be done at comparatively low-cost and in a repeatable environment within hardware-in-the-loop (HWIL) facilities. These HWIL stimulations help assess performance and reduce risks prior to full flight testing but come with several technical challenges. One such challenge is providing sensor stimuli that will result in realistic feedback to the avionics. Though aero-optical tools exist for predicting image distortions due to features of hypersonic flow fields, image degradation due to optical propagation through a heated and deformed window are missing. Because these thermal-structural effects can be critical for some designs, there is a need for real-time capable models suitable for closed-loop trajectory simulations that can capture both the aero-optical and thermal-structural distortions.Recognizing this need and opportunity, CFD Research Corporation in collaboration with Kinetics Incorporated proposes a workflow to provide a fast aero-optical and thermal-structural effects model that can be easily integrated with scene generators currently existing in hardware-in-the-loop facilities. Phase I will focus on: (1) generating databases of optical parameters using high-fidelity physics-based toolchains, (2) training surrogate models to predict these parameters, and (3) creating a GPU compatible application or FLITES plugin, to incorporate the optical effects into the scene generation pipeline.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

947 SBIR/STTR records share this UEI (1987–2026). Reported award amounts total $350,893,199. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Health and Human Services, National Science Foundation, Department of Commerce, Department of Energy

Agency intelligence

Department of Defense

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