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Alternatives for jet engine controlGeneral goals of the research were classified into two categories. The first category involves the use of modern multivariable frequency domain methods for control of engine models in the neighborhood of a quiescent point. The second category involves the use of nonlinear modelling and optimization techniques for control of engine models over a more extensive part of the flight envelope. In the frequency domain category, works were published in the areas of low-interaction design, polynomial design, and multiple setpoint studies. A number of these ideas progressed to the point at which they are starting to attract practical interest. In the nonlinear category, advances were made both in engine modelling and in the details associated with software for determination of time optimal controls. Nonlinear models for a two spool turbofan engine were expanded and refined; and a promising new approach to automatic model generation was placed under study. A two time scale scheme was developed to do two-dimensional dynamic programming, and an outward spiral sweep technique has greatly speeded convergence times in time optimal calculations.
Document ID
19780023164
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Leake, R. J.
(Notre Dame Univ. IN, United States)
Sain, M. K.
(Notre Dame Univ. IN, United States)
Date Acquired
September 3, 2013
Publication Date
February 28, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-157578
Report Number: NASA-CR-157578
Accession Number
78N31107
Funding Number(s)
CONTRACT_GRANT: NSG-3048
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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