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An application of modern control theory to jet propulsion systemsThe control of an airbreathing turbojet engine by an onboard digital computer is studied. The approach taken is to model the turbojet engine as a linear, multivariable system whose parameters vary with engine operating environment. From this model adaptive closed-loop or feedback control laws are designed and applied to the acceleration of the turbojet engine.
Document ID
19750015501
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Merrill, W. C. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1975
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-X-71726
Accession Number
75N23573
Funding Number(s)
CONTRACT_GRANT: NGR-36-010-024
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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