This paper provides an overview of the aircraft turbine engine
control research at the 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 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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