摘要: A flight test was conducted for preliminary evaluation of an aileron-rudder interconnect (ARI) control system for the F-14A airplane in the landing configuration. Two ARI configurations were tested in addition to the standard F-14... 展开
作者 | Kelley, W. W. Enevoldson, E. K. | ||
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原报告号 | N8213148 | 总页数 | 39 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Ailerons Aircraft landing Controllability F-14 aircraft Flight control Rudders Angle of attack Approach Circuit diagrams Directional control Flight tests Lateral control |