| タイトル | Simulation and flight studies of an approach profile indicator for VTOL aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760004969 |
| 著者（英） | Yenni, K. R.; Moen, G. C. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1975-11-01 |
| 言語 | eng |
| 内容記述 | Simulation and flight investigations were conducted by using a method of providing supplementary information to the pilot in conjunction with a closed-circuit-television display during a VTOL instrument final approach including deceleration and hover. The supplementary information included range, cross range, ground speed, altitude, and rate-of-climb error and was displayed on an instrument called an approach profile indicator. The display was arranged to provide both quasi-command and situation information. Pilot comments indicated that the approach-profile-indicator display concept in conjunction with the closed-circuit television resulted in a decreased pilot workload and an increase in pilot confidence. Also, the results indicated that the approach profile repeatability was significantly improved because of the ground-speed and altitude information provided on the approach profile indicator. |
| NASA分類 | AIRCRAFT INSTRUMENTATION |
| レポートNO | 76N12057
L-10204
NASA-TN-D-8051 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/187972 |
