Small Business Innovation Research/Small Business Tech Transfer
Distributed Engine Control Empirical/Analytical Verification Tools, Phase I
Project Introduction
In this Phase I project, Impact Technologies, in collaboration with Prof. R.K. Yedavalli, propose a novel verification environment for eventual rapid certification of distributed engine control systems (DCS). Our approach is focused on providing a set of tools to the government and industry that will allow faster certification of the control system as new high-temperature components and control laws are developed. A distributed hardware-in-the-loop (D-HIL) simulation tool is proposed to assist NASA and the Distributed Engine Control Working Group (DECWG) to integrate DCS components onto existing and next-generation engines. The proposed D-HIL simulator consist of a thermal test chamber operated by an engine simulation which is capable of subjecting components to a range of possible transient thermal conditions seen during engine operation , while functioning as elements in the networked control loop. To aid in certification of more complex distributed engine control hardware and software, a set of analysis tools is proposed. The Global Verification Toolset makes use of global stability and bounded verification methodologies to allow stability and performance to be assessed in a systematic fashion. At the conclusion of Phase I, the new verification facility and software tools will be demonstrated in a system test using the C-MAPSS engine.
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Anticipated Benefits
Aside from commercial aviation platforms, the application arena for distributed control system V&V tools extends to Air Force engine platforms. The verification toolset will benefit fly-by-wire systems sponsored by DoD such as UAVs, UGVs, and AUVs. Interest in fault-tolerant distributed control systems spans across many industries, particularly the automotive, energy, and manufacturing systems areas. The proposed distributed hardware-in-the-loop evaluation platform and verification software tools will enable the development of distributed aircraft propulsion control systems and flight control avionic systems. In addition to Fundamental Aeronautics, the developed tools extend to verification of flight-critical control and health management software and distributed avionics that are relevant to the Aviation Safety and Exploration Systems. Impact Technologies will position the hardware simulator for inclusion in future planned NASA/DoD-led Distributed Engine Control demonstrations.
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| Sikorsky Aircraft Corporation | Lead Organization | Industry | Stratford, Connecticut |
Glenn Research Center
(GRC)
|
Supporting Organization | NASA Center | Cleveland, Ohio |
Primary U.S. Work Locations
-
Connecticut
-
Ohio
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Organization:
- Sikorsky Aircraft Corporation
Responsible Program:
- Small Business Innovation Research/Small Business Tech Transfer
Project Management
Program Director:
Program Manager:
Principal Investigator:
Project Duration
Start: Feb 2011
End: Sep 2011
Technology Maturity (TRL)
| Start: | 2 |
| Current: | 4 |
| Estimated End: | 4 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TX01 Propulsion Systems
- TX01.1 Chemical Space Propulsion
- TX01.1.2 Earth Storable
Target Destinations
Earth, Foundational Knowledge
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This is a historic project that was completed before the creation of TechPort on October 1, 2012. Available data has been included. This record may contain less data than currently active projects.