| タイトル | Optimality study of a gust alleviation system for light wing-loading STOL aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760011053 |
| 著者（英） | Komoda, M. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1976-02-01 |
| 言語 | eng |
| 内容記述 | An analytical study was made of an optimal gust alleviation system that employs a vertical gust sensor mounted forward of an aircraft's center of gravity. Frequency domain optimization techniques were employed to synthesize the optimal filters that process the corrective signals to the flaps and elevator actuators. Special attention was given to evaluating the effectiveness of lead time, that is, the time by which relative wind sensor information should lead the actual encounter of the gust. The resulting filter is expressed as an implicit function of the prescribed control cost. A numerical example for a light wing loading STOL aircraft is included in which the optimal trade-off between performance and control cost is systematically studied. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 76N18141
NASA-TN-D-8180
A-5906 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/186999 |
