摘要: This work is extending the research accomplished on project NCC2-751. A newlyimplemented helicopter model has been used to simulate 25 flight configurations near hover for the UH-60 RASCAL aircraft. A new engine model has been ins... 展开
作者 | Biezad, D. J. | ||
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原报告号 | N9431203 | 总页数 | 30 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Dynamic response Feedback Flight control Helicopter control Hoveringstability Rotary wing aircraft Aircraft models Directional stability Flight simulation Aerodynamic stability Aircraft stability Decoupling Hovering Lateral control Yaw |