| タイトル | Optimization-based controller design for rotorcraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940010169 |
| 著者（英） | Tsing, N.-K.; Tits, A. L.; Tischler, M. B.; Fan, M. K. H.; Barlow, J. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1993-02-15 |
| 言語 | eng |
| 内容記述 | An optimization-based methodology for linear control system design is outlined by considering the design of a controller for a UH-60 rotorcraft in hover. A wide range of design specifications is taken into account: internal stability, decoupling between longitudinal and lateral motions, handling qualities, and rejection of windgusts. These specifications are investigated while taking into account physical limitations in the swashplate displacements and rates of displacement. The methodology crucially relies on user-machine interaction for tradeoff exploration. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 94N14642 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/116465 |
