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Performance seeking control (PSC) for the F-15 highly integrated digital electronic control (HIDEC) aircraftThe performance seeking control algorithm optimizes total propulsion system performance. This adaptive, model-based optimization algorithm has been successfully flight demonstrated on two engines with differing levels of degradation. Models of the engine, nozzle, and inlet produce reliable, accurate estimates of engine performance. But, because of an observability problem, component levels of degradation cannot be accurately determined. Depending on engine-specific operating characteristics PSC achieves various levels performance improvement. For example, engines with more deterioration typically operate at higher turbine temperatures than less deteriorated engines. Thus when the PSC maximum thrust mode is applied, for example, there will be less temperature margin available to be traded for increasing thrust.
Document ID
19950026599
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Orme, John S.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publication: An Electronic Workshop on the Performance Seeking Control and Propulsion Controlled Aircraft Results of the F-15 Highly Integrated Digital Electronic Control Flight Research Program
Subject Category
Aircraft Propulsion And Power
Accession Number
95N33020
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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