Design and hovering control of a twin rotor tail-sitter UAV

作     者：Wufan WANG Jihong ZHU Minchi KUANG Xiaming YUAN Yunfei TANG Yaqing LAI Lyujie CHEN Yunjie YANG 

作者机构：Department of Computer Science and Technology Tsinghua University 

出 版 物：《Science China(Information Sciences)》 (中国科学:信息科学(英文版))

年 卷 期：2019年第62卷第9期

页      面：185-187页

核心收录：

学科分类：0810[工学-信息与通信工程] 0808[工学-电气工程] 08[工学] 081105[工学-导航、制导与控制] 082503[工学-航空宇航制造工程] 0825[工学-航空宇航科学与技术] 0811[工学-控制科学与工程] 0812[工学-计算机科学与技术（可授工学、理学学位）] 

基　　金：supported by National Natural Science Foundation of China (Grant Nos. 61603210  61673240) 

主　　题：Design and hovering control of a twin rotor tail-sitter UAV pro 

摘      要：The tail-sitter unmanned aerial vehicles (UAVs)combine the vertical takeoff and landing (VTOL)capabilities of rotary-wing UAVs and the efficient long-distance flight capability of fixed-wing UAVs.When compared with other hybrid aircraft configurations such as tilt-rotor [1] and tilt-wing [2]UAVs, the tail-sitter UAV possesses the simplest configuration and requires no extra mechanisms for performing the VTOL maneuver. This brings several benefits including high payload and low susceptibility to malfunctions.