Aircraft Turbine Engine Control Research at NASA Glenn Research Center
Publication: Journal of Aerospace Engineering
Volume 26, Issue 2
Abstract
This paper provides an overview of the aircraft turbine engine control research at NASA Glenn Research Center (GRC). A brief introduction to the engine control problem is first provided with a description of the state-of-the-art control law structure. A historical aspect of engine control development since the 1940s is then provided with a special emphasis on the contributions of GRC. With the increased emphasis on aircraft safety, enhanced performance, and affordability, as well as the need to reduce the environmental impact of aircraft, there are many new challenges being faced by the designers of aircraft propulsion systems. The Controls and Dynamics Branch (CDB) at the GRC is leading and participating in various projects to develop advanced propulsion controls and diagnostics technologies that will help meet the challenging goals of NASA Aeronautics Research Mission programs. The rest of the paper provides an overview of the various CDB technology development activities in aircraft engine control and diagnostics, both current and some accomplished in the recent past. The motivation for each of the research efforts, the research approach, technical challenges, and the key progress to date are summarized.
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Information & Authors
Information
Published In
Journal of Aerospace Engineering
Volume 26 • Issue 2 • April 2013
Pages: 422 - 438
Copyright
© 2013 American Society of Civil Engineers.
History
Received: May 31, 2012
Accepted: Nov 15, 2012
Published online: Mar 15, 2013
Published in print: Apr 1, 2013
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