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タイトルSimulation of a cockpit-display concept for executing a wake-vortex avoidance procedure
本文(外部サイト)http://hdl.handle.net/2060/19840013474
著者(英)Abbott, T. S.
著者所属(英)NASA Langley Research Center
発行日1984-04-01
言語eng
内容記述A piloted simulation study has been undertaken to determine the feasibility and potential benefits of utilizing a forward-looking display to provide information that would enable aircraft to reduce their in-trail separation, and hence increase runway capacity, through the application of multiple glide-path approach techniques. This portion of the study was an initial exploration into a concept in which traffic information was added to a head-up display (HUD) format to allow the pilot to monitor the traffic situation and to self-space on a lead aircraft during a single glide-path approach task. The tests were conducted in a motion-base cockpit simulator configured as a current-generation transport aircraft and include the dynamic effects of the vortices generated by the lead aircraft. The information provided on the HUD included typical aircraft-guidance information and the current and past positions of the lead aircraft. Additionally, the displayed information provided self-separation cues which allowed the pilot to maintain separation on the lead aircraft. The results of this study indicate that the display concept could provide sufficient information to the pilot for traffic monitoring and self-separation.
NASA分類AIRCRAFT INSTRUMENTATION
レポートNO84N21542
NAS 1.60:2300
L-15736
NASA-TP-2300
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/159845


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