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Predicting dynamic performance limits for servosystems with saturating nonlinearitiesA generalized treatment for a system with a single saturating nonlinearity is presented and compared with frequency response plots obtained from an analog model of the system. Once the amplitude dynamics are predicted with the limit lines, an iterative technique is employed to determine the system phase response. The saturation limit line technique is used in conjunction with velocity and acceleration limits to predict the performance of an electro-hydraulic servosystem containing a single-stage servovalve. Good agreement was obtained between predicted performance and experimental data.
Document ID
19790020015
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Webb, J. A., Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Blech, R. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1979
Subject Category
Aircraft Stability And Control
Report/Patent Number
E-9903
NASA-TP-1488
Report Number: E-9903
Report Number: NASA-TP-1488
Accession Number
79N28186
Funding Number(s)
PROJECT: RTOP 505-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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