Abstract
The design of a robust digital multivariable feedback control system for the F-100 turbofan jet engine is considered. The control system design problem is posed, and conditions for satisfying performance specifications and stability robustness are stated. The discrete LQG/LTR methodology is used to design a compensator that meets the stated specifications. New results for multi-input LQR loop shaping are derived. To get a reasonably low-order compensator, frequency-weighted reduced-order models are exploited, with the reduction error treated as an uncertainty.
| Original language | English |
|---|---|
| Pages (from-to) | 363-383 |
| Number of pages | 21 |
| Journal | Dynamics and Control |
| Volume | 2 |
| Issue number | 4 |
| DOIs | |
| State | Published - Oct 1992 |
ASJC Scopus subject areas
- Control and Systems Engineering
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