| タイトル | A piloted simulator investigation of side-stick controller/stability and control augmentation system requirements for helicopter visual flight tasks |
| 著者（英） | Aiken, E. W.; Dunford, P. J.; Landis, K. H.; Hilbert, K. B. |
| 著者所属（英） | Boeing Vertol Co.|Army Research and Technology Labs. |
| 発行日 | 1984-01-01 |
| 言語 | eng |
| 内容記述 | A piloted simulator experiment was conducted to assess the effects of side-stick controller characteristics and level of stability and control augmentation on handling qualities for several low-altitude control tasks. Visual flight tasks were simulated using four-window computer-generated imagery depicting either a nap-of-the-earth course or a runway with obstacles positioned to provide a slalom course. Both low speed and forward flight control laws were implemented, and a method for automatically switching control modes was developed. Variations in force-deflection characteristics and the number of axes controlled through an integrated side-stick were investigated. With high levels of stability and control augmentation, a four-axis controller with small-deflection in all four axes achieved satisfactory handling qualities for low-speed tasks. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 84A46370 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/396516 |
