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