| タイトル | Nonlinear stability and control study of highly maneuverable high performance aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19910020836 |
| 著者（英） | Mohler, R. R. |
| 著者所属（英） | Oregon State Univ. |
| 発行日 | 1991-08-12 |
| 言語 | eng |
| 内容記述 | The purpose was to develop and apply new nonlinear system methodologies to the stability analysis and adaptive control of high angle of attack (alpha) aircraft such as the F-18. Considerable progress is documented on nonlinear adaptive control and associated model development, identification, and simulation. The analysis considered linear and nonlinear, longitudinal, high alpha aircraft dynamics with varying degrees of approximation dependent on the purpose. In all cases, angle of attack or pitch rate was controlled primarily by a horizontal stabilizer. In most cases studied, a linear adaptive controller provided sufficient stability. However, it has been demonstrated by simulation of a simplified nonlinear model that certain large rapid maneuvers were not readily stabilized by the investigated linear adaptive control, but were controlled instead by means of a nonlinear time-series based adaptive control. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 91N30150
OSU-ECE-91-01
NASA-CR-188721
NAS 1.26:188721 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/131260 |
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