Mode Transition Control of Dual Tilt Rotor Unmanned Aerial Vehicle Based on Dynamic Analysis

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	Mode Transition Control of Dual Tilt Rotor Unmanned Aerial Vehicle Based on Dynamic Analysis
	Zheng RJ(郑锐剑)1,2,3; He YQ(何玉庆)2,3; Liu Z(刘重)2,3,4; Yang LY(杨丽英)2,3; Gu F(谷丰)2,3
	2020
会议日期	August 22-24, 2020
会议地点	Hefei, China
关键词	Tilt Rotor Unmanned Aerial Vehicle Dynamic Analysis Model Transition Control Passivity
页码	1528-1533
英文摘要	To achieve the mode transition of a dual tilt rotor unmanned aerial vehicle (dual-TRUAV) from helicopter mode to airplane mode, this study focuses on its transition control method based on necessary dynamic analysis. The dynamic characteristics of the dual-TRUAV especially the longitudinal dynamics are simplified and analyzed mainly, where the influence of the rotor tilt angle on dual-TRUAV dynamics is emphasized. With the above dynamic analysis, the transition control strategy based on the rotor tilt angle is established. The stability analysis of the system with the designed control method is carried out via passive theory, and some simulation results are displayed to validate the control effectiveness.
源文献作者	IEEE Control Systems Society (CSS) ; Northeastern University ; State Key Laboratory of Synthetical Automation for Process Industries ; Technical Committee on Control Theory, Chinese Association of Automation
产权排序	1
会议录	Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020
会议录出版者	IEEE
会议录出版地	New York
语种	英语
ISBN号	978-1-7281-5854-9
WOS记录号	WOS:000621616901110
内容类型	会议论文
源URL	[http://ir.sia.cn/handle/173321/27699]
专题	沈阳自动化研究所_机器人学研究室
通讯作者	Zheng RJ(郑锐剑)
作者单位	1.College of Information Science and Engineering, Northeastern University, Shenyang 110819, China 2.State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, China 3.Institutes for Robotics and Intelligent Manufacturing, Chinese Academy of Sciences, Shenyang 110169, China 4.University of Chinese Academy of Sciences, Beijing 100049, China
推荐引用方式 GB/T 7714	Zheng RJ,He YQ,Liu Z,et al. Mode Transition Control of Dual Tilt Rotor Unmanned Aerial Vehicle Based on Dynamic Analysis[C]. 见:. Hefei, China. August 22-24, 2020.