| タイトル | A piloted simulation investigation of the normal load factor and longitudinal thrust required for air-to-air acquisition and tracking |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940008828 |
| 著者（英） | Whalley, Matthew S. |
| 著者所属（英） | Army Aviation Systems Command |
| 発行日 | 1993-07-01 |
| 言語 | eng |
| 内容記述 | A piloted simulation study was performed by the U.S. Army Aeroflighydynamics Directorate to develop insight into the maneuverability requirements for aggressive helicopter maneuvering tasks such as air-to-air combat. Both a conventional helicopter and a helicopter with auxiliary thrust were examined. The aircraft parameters of interest were the normal and longitudinal load factor envelopes. Of particular interest were the mission performance and handling qualities tradeoffs with the parameters of interest. Two air-to-air acquisition and tracking tasks and a return-to-cover task were performed to assess mission performance. Results indicate that without auxiliary thrust, the ownship normal load factor capability needs to match that of the adversary in order to provide satisfactory handling qualities. Auxiliary thrust provides significant handling qualities advantages and can be substituted to some extent for normal load factor capability. Auxiliary thrust levels as low as 0.2 thrust/weight can provide significant handling qualities advantages. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 94N13301 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/116846 |
