| タイトル | Simulator evaluation of a display for a Takeoff Performance Monitoring System |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890014098 |
| 著者（英） | Middleton, David B.; Person, Lee H., Jr.; Srivatsan, Raghavachari |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1989-05-01 |
| 言語 | eng |
| 内容記述 | A Takeoff Performance Monitoring System (TOPMS) has been developed to provide the pilot with graphic and numeric information pertinent to his decision to continue or abort a takeoff. The TOPMS information display consists primarily of a runway graphic overlaid with symbolic status, situation, and advisory information including: (1) current position and airspeed; (2) predicted locations for reaching decision speed (V sub 1) and rotation speed (V sub R); (3) groundroll limit for reaching (V sub R); (4) predicted stop point for an aborted takeoff from current conditions; (5) engine-status flags; and (6) an overall situation advisory flag that recommends continuation or rejection of the takeoff. In this study, 32 experienced multi-engine pilots evaluated the TOPMS on the Langley B-737 real-time research simulator. They rated the system satisfactory - good and judged it to be suitable for implementation on an aircraft. The TOPMS, the TOPMS simulation, and the results of the simulator evaluation are described here. Appendices contain the pilot's prebriefing package (written explanation of the TOPMS--sent to the pilots prior to their visit), evaluation instructions, debriefing questions, and rating criteria (organized into a flow diagram similar to the Cooper-Harper diagram for evaluation of aircraft handling qualities). |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 89N23469
L-16510
NAS 1.60:2908
NASA-TP-2908 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/142064 |
