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A sensitivity analysis for the F100 turbofan engine using the multivariable Nyquist arrayIn the feedback control design of multivariable systems, closed loop performance evaluations must include the dynamic behavior of variables unavailable to the feedback controller. For the multivariable Nyquist array method, a set of sensitivity functions are proposed to simplify the adjustment of compensator parameters when the dynamic response of the unmeasurable output variables is unacceptable. A sensitivity study to improve thrust and turbine temperature responses for the Pratt-Whitney F100 turbofan engine demonstrates the utility of the proposed method.
Document ID
19790039784
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Leininger, G. G.
(Toledo Univ. OH, United States)
Borysiak, M. L.
(Toledo, University Toledo, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: Modeling and simulation. Volume 9 - Ninth Annual Pittsburgh Conference
Location: Pittsburgh, PA
Start Date: April 27, 1978
End Date: April 28, 1978
Accession Number
79A23797
Funding Number(s)
CONTRACT_GRANT: NSG-3171
CONTRACT_GRANT: NSG-3084
Distribution Limits
Public
Copyright
Other

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