| タイトル | Practical optimal flight control system design for helicopter aircraft. Volume 1: Technical Report |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800014839 |
| 著者（英） | Riedel, S. A.; Hofmann, L. G.; Mcruer, D. |
| 著者所属（英） | Systems Technology, Inc. |
| 発行日 | 1980-05-01 |
| 言語 | eng |
| 内容記述 | A method by which modern and classical theory techniques may be integrated in a synergistic fashion and used in the design of practical flight control systems is presented. A general procedure is developed, and several illustrative examples are included. Emphasis is placed not only on the synthesis of the design, but on the assessment of the results as well. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 80N23328
TR-1127-1-I
NASA-CR-3275 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/172615 |
