摘要: The effects of significant control system dynamics on fighter approach and landing longitudinal flying qualities were investigated in flight using the USAF/Calspan variable stability NT-33 aircraft. Two pilots evaluated 49 differe... 展开
作者 | smith,rogers e. | ||
---|---|---|---|
原报告号 | ADA067550 | 总页数 | 232 |
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Flight control systems Aircraft landings Fly by wire control Digital systems Approach Aerodynamic characteristics Jet fighters Pitch(Motion) Variable stability aircraft Jet training planes Test vehicles Flight Quality Flight testing Data bases T-33 aircraft NT-33 aircraft Flying qualities |