| タイトル | Simulator study of pilot-aircraft-display system response obtained with a three-dimensional-box pictorial display |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840005114 |
| 著者（英） | Adams, J. J. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1983-12-01 |
| 言語 | eng |
| 内容記述 | The effect of varying the two important display parameters of a pictorial display on pilot opinion performance, and pilot aircraft display system servomechanism response is examined. The display presents a picture of a three dimensional box that moves along the desired path ahead of the aircraft. The two display parameters examined are the field of view of the picture (from + or - 5 deg to + or - 45 deg) and the distance to the box (from 92 m (300 ft) to 6100 m (20 000 ft)). The results show that the pilots prefer a distance to the box of 915 m (3000 ft) and a field of view of + or - 30 deg. The best performance, both in the sense of quickness of error correction and lowest standard deviation, is obtained with a distance to the box of 92 m (300 ft) and a field of view of + or - 15 deg. A pilot model analysis is used to determine the gains used by the pilots and the servomechanism response characteristics of the pilot aircraft display system. |
| NASA分類 | AIRCRAFT INSTRUMENTATION |
| レポートNO | 84N13182
NAS 1.60:2122
L-15632
NASA-TP-2122 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/160963 |
