| タイトル | Robust control design techniques for active flutter suppression |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940031368 |
| 著者（英） | Ozbay, Hitay; Bachmann, Glen R. |
| 著者所属（英） | Ohio State Univ. |
| 発行日 | 1994-06-01 |
| 言語 | eng |
| 内容記述 | In this paper, an active flutter suppression problem is studied for a thin airfoil in unsteady aerodynamics. The mathematical model of this system is infinite dimensional because of Theodorsen's function which is irrational. Several second order approximations of Theodorsen's function are compared. A finite dimensional model is obtained from such an approximation. We use H infinity control techniques to find a robustly stabilizing controller for active flutter suppression. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 94N35875 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/111282 |
