摘要: Six-degree-of-freedom ground-based and in-flight simulator studies were conducted to evaluate the low-speed flight characteristics of a twin-fuselage passenger transport airplane and to compare these characteristics with those of ... 展开
作者 | Grantham, W. D. Smith, P. M. Neely, W. R. Deal, P. L. Yenni, K. R. | ||
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原报告号 | N8534144 | 总页数 | 55 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Approach Controllability Flight characteristics Fuselages Landing Transport aircraft Degrees of freedom Control systems design Flight simulation Pilot performance |