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Multivariable control for the F-100 engine using the LQG/LTR methodologyThe design of a multivariable feedback control system for the Pratt and Whitney F-100 turbofan jet engine is a challenging task for control engineers. This paper employs a linearized model of the F-100 engine to demonstrate the use of the newly developed Linear Quadratic Gaussian/Loop Transfer Recovery (LQG/LTR) design methodology, which adopts an integrated frequency-domain and time-domain approach to multivariable feedback control synthesis so as to meet stability-robustness, command-following, and disturbance-rejection specifications.
Document ID
19840060663
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Athans, M.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Kapasouris, P.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Kappos, E.
(MIT Cambridge, MA, United States)
Spang, H. A., III
(MIT, Cambridge, MA; GE Corporate Research and Development Center Schenectady, NY, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 84-1910
Accession Number
84A43450
Funding Number(s)
CONTRACT_GRANT: NGL-22-009-124
Distribution Limits
Public
Copyright
Other

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