| タイトル | Application of variable structure system theory to aircraft flight control |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810014560 |
| 著者（英） | Calise, A. J.; Kramer, F.; Kadushin, I. |
| 著者所属（英） | Drexel Univ. |
| 発行日 | 1981-05-01 |
| 言語 | eng |
| 内容記述 | The current status of research on the application of variable structure system (VSS) theory to design aircraft flight control systems is summarized. Two aircraft types are currently being investigated: the Augmentor Wing Jet STOL Research Aircraft (AWJSRA), and AV-8A Harrier. The AWJSRA design considers automatic control of longitudinal dynamics during the landing phase. The main task for the AWJSRA is to design an automatic landing system that captures and tracks a localizer beam. The control task for the AV-8A is to track velocity commands in a hovering flight configuration. Much effort was devoted to developing computer programs that are needed to carry out VSS design in a multivariable frame work, and in becoming familiar with the dynamics and control problems associated with the aircraft types under investigation. Numerous VSS design schemes were explored, particularly for the AWJSRA. The approaches that appear best suited for these aircraft types are presented. Examples are given of the numerical results currently being generated. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 81N23093
NASA-CR-164321 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/169221 |
