NASA NTRS · 19840060663
Multivariable control for the F-100 engine using the LQG/LTR methodology
Abstract
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.
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Athans, M., Kapasouris, P., Kappos, E., Spang, H. A., III. 1984-01-01. Multivariable control for the F-100 engine using the LQG/LTR methodology. https://ntrs.nasa.gov/citations/19840060663
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