Linear-quadratic Gaussian with loop-transfer recovery methodology for the F-100 engine
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Athans, M.↗
Engineering topics
Kappos, E.
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Multivariable control for the F-100 engine using the LQG/LTR methodology
The 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.
Athans, M.↗