| タイトル | Performance seeking controls |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810003582 |
| 著者（英） | Seldner, K. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1980-10-01 |
| 言語 | eng |
| 内容記述 | A performance logic algorithm (PSL) was developed to optimize the performance of propulsion systems for component and sensor degradations by monitoring the performance of the engine system and minimizing thrust specific fuel consumption (TSFC) while retaining a constant engine net thrust. Engine constraints such as surge margin, speed, pressure, and temperature are observed. The PSL algorithm was applied to the quiet, clean, short haul experimental engine. Engine control set points were modified for component degradations in order to restore the nominal net thrust. Results show convergence to the optimum value can be obtained within 60 to 90 seconds, which makes the program acceptable to on line operation with present state of the art minicomputers. Tests indicate that in most cases the PSL algorithm offers some improvement in thrust specific fuel consumption over the manual throttle. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 81N12092 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/568417 |
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