SBIR/STTR Research Award

Predictive Model Based Control System for High Speed Dynamic Airframe Testing Solution

Award identifier 84461748707f480d28d3b08e296807fbc8827bdd35cb6177d7928069b0f1440fAwarding agency Department of Defense · Navy

Award amount

$139,879

Program and phase

SBIR · Phase I

Award year

2021

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Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
DAYTON T. BROWN, INC.
Proposal award date
2021-08-04
Contract end date
2022-02-07
UEI
GN84UHWZJMR8
Solicitation number
21.1
Topic code
N211-014

Research abstract

The physical testing of airframe designs is a vital component of ensuring their safety, reducing their long term costs and providing a robust platform that has long term fleet readiness. In order to be of the most value, an airframe fatigue test must not only accurately apply the proper loads to the structure, but must also do this in a time frame where the findings can be of value. Improvements to the design need to be introduced into production and retrofitted to the fleet early in the fleet’s life in order to provide the most benefit. The current established fatigue methodology can only apply loads at rates far slower than the load cycles accumulate on rotorcraft and therefore rely on spectrum truncation and load adjustments to theoretically match the fatigue damage. However there is evidence that this methodology results in unconservative crack growth rates. The test load cycle rate needs to be greatly accelerated in order to apply realistic loads, in a reasonable amount of test time. In order to accelerate the fatigue test, and to obtain more value from it, all aspects of the test system must be reexamined and improved. This includes the spectrum development, the load control system, load application methods, data acquisition and test monitoring. The key innovation proposed for the topic is to combine the knowledge from the DTB developed adaptive load control algorithm with a proven MIL (Model in the Loop) algorithm, to enable the load control system to respond in a predictable manner to large load / deflection loadings while adapting the load application parameters to adjust to nonlinear effects. DTB will bring to the table as team leader our years of structural testing experience. DTB is familiar with all aspects of airframe structural testing and will use this knowledge to integrate a solution based on inputs from all team members. We have formed an expert team including load control system developers and control system modeling experts to determine a framework for a complete implementation of a scalable, real-time, predictive, and adaptive model-based test frame control system that increases load cycling frequency while maintaining load accuracy.

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

11 SBIR/STTR records share this UEI (2012–2021). Reported award amounts total $2,927,847. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense

Agency intelligence

Department of Defense

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