摘要: A flight evaluation was conducted to determine the effect of engine throttleresponse characteristics on precision formation-flying qualities. A variable electronic throttle control system was developed and flight-tested on a TF-10... 展开
作者 | Walsh, K. R. | ||
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原报告号 | N9323123 | 总页数 | 26 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aircraft engines Engine control F-104 aircraft Flight characteristics Throttling Thrust Electronic control Flight tests Fuel control Time lag Aircraft control Control systems design Controllability Engine design Time dependence |