Aircraft Turbine Engine Control Research at NASA Glenn Research Center
Author:
Affiliation:
1. Chief, Controls and Dynamics Branch, National Aeronautics and Space Administration Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135.
Publisher
American Society of Civil Engineers (ASCE)
Subject
Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering
Link
http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000296
Reference47 articles.
1. Adibhatla S. and Lewis T. (1997). “Model-based intelligent digital engine control (MoBIDEC).” 97-3192 American Institute of Aeronautics and Astronautics Reston VA.
2. Bright M. M. et al. (1994). “Piloted evaluation of an integrated methodology for propulsion and airframe control design.” 94-3612 American Institute of Aeronautics and Astronautics Reston VA.
3. Stall Precursor Identification in High-Speed Compressor Stages Using Chaotic Time Series Analysis Methods
4. Burcham F. W. et al. (1984). “Digital engine electronic control (DEEC) flight evaluation in an F–15 airplane.” CP-2298 NASA Washington DC.
5. Culley D. E. (2010). “Transition in gas turbine control system architecture: Modular distributed and embedded.” GT2010-23226 ASME New York.
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