| タイトル | Nonlinear control of aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19860019486 |
| 著者（英） | Hunt, L. R.; Meyer, G.; Su, R. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1984-01-01 |
| 言語 | eng |
| 内容記述 | Transformations of nonlinear systems were used to design automatic flight controllers for vertical and short takeoff aircraft. Under the assumption that a nonlinear system can be mapped to a controllable linear system, a method using partial differential equations was constructed to approximate transformations in cases where exact ones cannot be found. An application of the design theory to a rotorcraft, the UH-1H helicopter, was presented. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 86N28958
NASA-TM-89225
NAS 1.15:89225 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/153662 |
