| タイトル | Multivariable control for the F-100 engine using the LQG/LTR methodology |
| 著者（英） | Spang, H. A., III; Athans, M.; Kappos, E.; Kapasouris, P. |
| 著者所属（英） | General Electric Co.|Massachusetts Inst. of Tech. |
| 発行日 | 1984-01-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 84A43450
AIAA PAPER 84-1910 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/396894 |
