摘要: The purpose of this report is to determine the applicability of the QuantitativeFeedback Theory (QFT) approach to designing the control laws for a modern military flight control system. This report documents a portion of the QFT r... 展开
作者 | Sheldon, S. N. | ||
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原报告号 | ADA339188 | 总页数 | 99 |
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Flight control systems Jet fighters Flight simulation Aerodynamic stability Flight envelope Control theory Flight simulators Flight maneuvers Subsonic flight |