| タイトル | Integrated aeroservoelastic tailoring of lifting surfaces |
| 著者（英） | Weisshaar, T. A.; Zeiler, T. A. |
| 著者所属（英） | Purdue Univ.|PRC Kentron, Inc. |
| 発行日 | 1986-01-01 |
| 言語 | eng |
| 内容記述 | An approach to the integration of two design activities, structural design and active control design, for a highly idealized aeroservoelastic system is presented. The particular design goal for this study is the maximization of the stable airspeed envelope of an idealized model of an aeroservoelastic system through rational and systematic variation of structural and control design parameters. The steady-state linear quadratic regulator is used to model the control subsystem; the structural subsystem is assigned characteristic design parameters, such as shear center position. The application of the procedure described here produces optimally controlled structures with stability characteristics superior to those of open-loop and initial closed-loop designs. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 86A38946
AIAA PAPER 86-1005 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/384342 |
