| タイトル | Quadratic synthesis of integrated active controls for an aeroelastic forward-swept-wing-aircraft |
| 著者（英） | Schmidt, D. K.; Gilbert, M. G.; Weisshaar, T. A. |
| 著者所属（英） | Purdue Univ. |
| 発行日 | 1982-01-01 |
| 言語 | eng |
| 内容記述 | State variable representations of flexible aircraft are obtained using a modeling approach which first defines a mean-reference axis coordinate system. The active system design approach for forward-swept-wing aircraft also expresses structural deformations of the wing in terms of free normal vibration modes relative to this mean reference axis. Calculations which assume quasi-steady incompressible aerodynamics are performed to obtain generalized force expressions for flight conditions. The use of this quadratic synthesis technique shows that increased performance and redundancy over decentralized approaches can be achieved using integrated active longitudinal stability augmentation and aeroelastic stabilization. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 83A12458
AIAA PAPER 82-1544 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/406863 |
