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Control of propulsion systems for supersonic cruise aircraftThe propulsion control requirements of supersonic aircraft are presented. Integration of inlet, engine, and airframe controls is discussed. The application of recent control theory developments to propulsion control design is described. Control component designs for achieving reliable, responsive propulsion control are also discussed.
Document ID
19770011072
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hiller, K. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Drain, D. I.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: Proc. of the SCAR Conf., Part 1
Subject Category
Aircraft Propulsion And Power
Accession Number
77N18016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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