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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
Department机器人学研究室
Conference Name32nd Chinese Control and Decision Conference, CCDC 2020
Conference DateAugust 22-24, 2020
Conference PlaceHefei, China
Author of SourceIEEE Control Systems Society (CSS) ; Northeastern University ; State Key Laboratory of Synthetical Automation for Process Industries ; Technical Committee on Control Theory, Chinese Association of Automation
Source PublicationProceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020
PublisherIEEE
Publication PlaceNew York
2020
Pages1528-1533
Indexed ByEI
EI Accession number20204009255245
Contribution Rank1
ISBN978-1-7281-5854-9
KeywordTilt Rotor Unmanned Aerial Vehicle Dynamic Analysis Model Transition Control Passivity
AbstractTo 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.
Language英语
Document Type会议论文
Identifierhttp://ir.sia.cn/handle/173321/27699
Collection机器人学研究室
Corresponding AuthorZheng RJ(郑锐剑)
Affiliation1.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
Recommended Citation
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]//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. New York:IEEE,2020:1528-1533.
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