| タイトル | Landing flying qualities evaluation criteria for augmented aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810005458 |
| 著者（英） | Smith, R.; Radford, R. C.; Bailey, R. |
| 著者所属（英） | Calspan Advanced Technology Center |
| 発行日 | 1980-06-01 |
| 言語 | eng |
| 内容記述 | The criteria evaluated were: Calspan Neal-Smith; Onstott (Northrop Time Domain); McDonnell-Douglas Equivalent System Approach; R. H. Smith Criterion. Each criterion was applied to the same set of longitudinal approach and landing flying qualities data. A revised version of the Neal-Smith criterion which is applicable to the landing task was developed and tested against other landing flying qualities data. Results indicated that both the revised Neal-Smith criterion and the Equivalent System Approach are good discriminators of pitch landing flying qualities; Neal-Smith has particular merit as a design guide, while the Equivalent System Approach is well suited for development of appropriate military specification requirements applicable to highly augmented aircraft. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 81N13969
CALSPAN-6339-F-3
NASA-CR-163097 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/170520 |
