摘要: An inflight research study was conducted utilizing the USAF Total Inflight Simulator (TIFS) to investigate longitudinal flying qualities for the flared landing approach phase of flight. The purpose of the experiment was to generat... 展开
作者 | weingarten, n. c. berthe, c. j. | ||
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原报告号 | N8715234 | 总页数 | 200 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aircraft control Aircraft stability Flight characteristics Landing aids Controllability Aircraft landing Flight simulators Performance prediction Pilot performance Pitch (Inclination) Time dependence |