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A real-time simulator of a turbofan engineA real-time digital simulator of a Pratt and Whitney F100 engine has been developed for real-time code verification and for actuator diagnosis during full-scale engine testing. This self-contained unit can operate in an open-loop stand-alone mode or as part of closed-loop control system. It can also be used for control system design and development. Tests conducted in conjunction with the NASA Advanced Detection, Isolation, and Accommodation program show that the simulator is a valuable tool for real-time code verification and as a real-time actuator simulator for actuator fault diagnosis. Although currently a small perturbation model, advances in microprocessor hardware should allow the simulator to evolve into a real-time, full-envelope, full engine simulation.
Document ID
19890011624
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Litt, Jonathan S.
(Army Aviation Research and Development Command Cleveland, OH., United States)
Delaat, John C.
(NASA Lewis Research Center Cleveland, OH, United States)
Merrill, Walter C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1989
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-4578
AVSCOM-TR-89-C-001
AD-A206830
NAS 1.15:100869
NASA-TM-100869
Report Number: E-4578
Report Number: AVSCOM-TR-89-C-001
Report Number: AD-A206830
Report Number: NAS 1.15:100869
Report Number: NASA-TM-100869
Accession Number
89N20995
Funding Number(s)
PROJECT: RTOP 505-62-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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