摘要: Flight tests were carried out to assess the feasibility of piloted steep curved, and decelerating approach profiles in powered lift STOL aircraft. Several STOL control concepts representative of a variety of aircraft were evaluate... 展开
作者 | hindson, w. s. hardy, g. h. | ||
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原报告号 | N8119131 | 总页数 | 96 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aircraft landing Approach control Flight tests Instrument landing systems Manual control Short takeoff aircraft Aircraft guidance Avionics Configuration management Descent Energy conservation Flight control Navigation |