摘要: A method, called pseudo controls, of integrating several airplane controls to achieve cooperative operation is presented. The method eliminates conflicting control motions, minimizes the number of feedback control gains, and reduc... 展开
作者 | Lallman, F. J. Davidson, J. B. Murphy, P. C. | ||
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原报告号 | N19980232887 | 总页数 | 44 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Thrust vector control Fighter aircraft Flight control Feedback control Directional control Control stability Angular acceleration Angle of attack F-18 aircraft Vanes Strakes Stability Forebodies Control surfaces Aerodynamics |