摘要: A systematic analytical approach to the determination of helicopter IFR precision approach requirements is formulated. The approach is based upon the hypothesis that pilot acceptance level or opinion rating of a given system is in... 展开
作者 | Phatak, A. V. | ||
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原报告号 | N80-28330 | 总页数 | 124 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Approach control Glide paths Helicopter control Instrument flight rules Landing simulation Pilot performance Aircraft landing All-weather landing systems Man machine systems Task complexity Uh-1 helicopter |