摘要: An in-flight investigation of the flying qualities of a twin fuselage aircraft design in the approach and landing flight phase was carried out in the USAF/AFWAL Total In-Flight Simulator (TIFS). The objective was to determine the ... 展开
作者 | Weingarten, N. C. | ||
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原报告号 | N8513801 | 总页数 | 87 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aircraft configurations Aircraft landing Approach Cues Flight characteristics Flight simulation Fuselages Pilot performance Visual stimuli Aircraft control Aircraft maneuvers Roll Transport aircraft |