摘要: An advanced methodology for integrated flight propulsion control (IFPC) designfor future aircraft, which will use propulsion system generated forces and moments for enhanced maneuver capabilities, is briefly described. This method... 展开
作者 | Garg, S. Mattern, D. | ||
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原报告号 | N9511159 | 总页数 | 17 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Control systems design Flight control Stovl aircraft Thrust control Transition flight Turbojet engine control Aircraft landing Hovering Maneuverability Vertical landing |