| タイトル | Design for active flutter suppression and gust alleviation using state-space aeroelastic modeling |
| 著者（英） | Karpel, M. |
| 著者所属（英） | Stanford Univ. |
| 発行日 | 1980-01-01 |
| 言語 | eng |
| 内容記述 | An analytical design technique for an active flutter-suppression and gust-alleviation control system is presented. It is based on a rational approximation of the unsteady aerodynamic loads in the entire Laplace domain, which yields matrix equations of motion with constant coefficients. Some existing rational approximation schemes are reviewed, and a new technique which yields a minimal number of augmented states for a desired accuracy is presented. The state-space aeroelastic model is used to design a constant gain, partial-feedback control system, which simultaneously assures stability and optimizes any desired combination of gust response parameters throughout the entire flight envelope. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 80A35058
AIAA PAPER 80-0766 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/421886 |
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