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Interaction studies on a jet engine model by characteristic methodologiesIt is shown how the generalized characteristic locus method developed by MacFarlane (1972) can be used for the step-by-step design of multivariable closed-loop compensators. The design procedure attempts to strike a balance between four conflicting objectives: stability, integrity, interaction, and accuracy. The generalized locus method is illustrated by a jet engine example.
Document ID
19770046529
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Seshadri, V.
(Notre Dame Univ. IN, United States)
Sain, M. K.
(Notre Dame, University Notre Dame, Ind., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: Midwest Symposium on Circuits and Systems
Location: Milwaukee, WI
Start Date: August 16, 1976
End Date: August 17, 1976
Accession Number
77A29381
Funding Number(s)
CONTRACT_GRANT: NSG-3048
CONTRACT_GRANT: NSF ENG-75-22322
Distribution Limits
Public
Copyright
Other

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