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	Flight dynamics study of a small tilt rotor UAV with tail propeller
	Wu, D.; Li, H.; Li, S.
	2016
会议名称	16th AIAA Aviation Technology, Integration, and Operations Conference
关键词	Aviation Conceptual design Design Flight dynamics Genetic algorithms Propellers Turbomachine blades Unmanned aerial vehicles (UAV) Dynamics studies Flight dynamics model Flying quality Multi-body dynamic Simulation model Slipstream effects Tilt-rotor aircrafts Transition flight Convertible helicopters
URL标识	查看原文
内容类型	会议论文
URI标识	http://www.corc.org.cn/handle/1471x/5957194
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Wu, D.,Li, H.,Li, S.. Flight dynamics study of a small tilt rotor UAV with tail propeller[C]. 见:16th AIAA Aviation Technology, Integration, and Operations Conference.

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