SBIR/STTR Research Award

Model-Free Control System for Scramjet Applications

Award identifier 18e34815b4f6554269cf3978cceb7837ac05a92e72196e4726cd3392e241d67bAwarding agency Department of Defense · Air Force

Award amount

$99,988

Program and phase

SBIR · Phase I

Award year

2009

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
COMPUTATIONAL SCIENCES LLC
Proposal award date
2009-03-23
Contract end date
2009-12-23
UEI
PYVAK1B5N7W4
Solicitation number
2008.3
Topic code
AF083-121

Research abstract

Flow fluctuations in the flame-holder cavity affect its stable operation that can lead to degradation of its performance. Efficient cavity operations can be enhanced through active control of injection of air and fuel mixtures. We propose to design and validate a novel Model-Free Direct (feedback) Control system to ensure stable cavity operation in the subsonic regime with smooth transitions to supersonic combustion. We will focus on a model-free strategy interacting with sensor and actuator arrays. Control system design and prototyping will be done with the aid of an existing simulation environment that connects flow solvers acting as plant emulators to control software. This approach will allow full accounting of the interaction of sensor-controller-actuator-flow dynamics in an active flow control loop.  Phase I will focus sensor-controller-actuator model preparation, design of numerical experiments for control system testing, and simulation of combustor operations for testing of control system performance. The testing will involve control software-in-the-loop and control hardware-in-the-loop simulations. The response of flowfield to variations in the sensor-controller-actuator configurations will be evaluated.  Phase II work will oversee the refinement of the existing control hardware prototype.  Phase III commercialization will seek to exploit the natural dual-use applicability of the developed hardware. BENEFIT: In addition to military use, the generality of the controller design will be suitable for multi-use applications. Immediate use relates to optimization of flame-holder operations, and prevention of isolator unstart in scramjet combustors. It will also benefit areas where distributed flow control is of interest including: aerospace (L/D and maneuverability optimization), maritime (wake signature minimization), and automotive (combustion efficiency maximization). Controller hardware will be interfaceable with personal computers using low-cost PCI boards. Such an interface will allow for very efficient virtual prototyping of complete control systems.

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 (2007–2015). Reported award amounts total $3,733,111. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense

Agency intelligence

Department of Defense

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