摘要: A modular flight control system is developed for a tailless fighter aircraft with innovative control effectors. Dynamic inversion control synthesis is used to develop a full envelope flight control law. Minor dynamic inversion com... 展开
作者 | Buffington, J. F. | ||
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原报告号 | ADA374954 | 总页数 | 154 |
主办者 | Non Paid ADAS | ||
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Aerodynamic configurations Fighter aircraft Tailless aircraft Flight control systems Aerodynamic stability Flight envelope Flight maneuvers Aircraft models Flight simulation |