NASA NTRS · 19770046529
Interaction studies on a jet engine model by characteristic methodologies
Abstract
It 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.
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Seshadri, V., Sain, M. K.. 1976-01-01. Interaction studies on a jet engine model by characteristic methodologies. https://ntrs.nasa.gov/citations/19770046529
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