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Performance seeking controlsA performance logic algorithm (PSL) was developed to optimize the performance of propulsion systems for component and sensor degradations by monitoring the performance of the engine system and minimizing thrust specific fuel consumption (TSFC) while retaining a constant engine net thrust. Engine constraints such as surge margin, speed, pressure, and temperature are observed. The PSL algorithm was applied to the quiet, clean, short haul experimental engine. Engine control set points were modified for component degradations in order to restore the nominal net thrust. Results show convergence to the optimum value can be obtained within 60 to 90 seconds, which makes the program acceptable to on line operation with present state of the art minicomputers. Tests indicate that in most cases the PSL algorithm offers some improvement in thrust specific fuel consumption over the manual throttle.
Document ID
19810003582
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Seldner, K.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1980
Publication Information
Publication: Propulsion Controls, 1979
Subject Category
Aircraft Propulsion And Power
Accession Number
81N12092
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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