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Alternatives for jet engine controlAlternatives to linear quadratic regulator theory in the linear case are examined along with nonlinear modelling and optimization approaches for global control. Context for the studies has been set by the DYNGEN digital simulator and by models generated for various phases of the F100 Multivariable Control Synthesis Program. With respect to the linear alternatives, the multivariable frequency domain is stressed. Progress is reported in both the direct algebraic approach to exact model matching, by means of stimulating work on the basic computational issues, and in the indirect generalized Nyquist approach. With respect to nonlinear modelling and optimization, the emphasis is twofold: the development of analytical nonlinear models of the jet engine and the use of these models in conjunction with techniques of mathematical programming in order to study global control over nonincremental portions of the flight envelope. The possibility of using tensor methods is explored.
Document ID
19810003593
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sain, M. K.
(Notre Dame Univ. IN, United States)
Schafer, R. M.
(Notre Dame Univ. IN, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1980
Publication Information
Publication: NASA. Lewis Research Center Propulsion Controls, 1979
Subject Category
Aircraft Propulsion And Power
Accession Number
81N12103
Funding Number(s)
CONTRACT_GRANT: NSG-3048
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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