Mode Transition Control of Dual Tilt Rotor Unmanned Aerial Vehicle Based on Dynamic Analysis
文献类型：会议论文
| 作者 | Zheng RJ(郑锐剑)1,2,3; He YQ(何玉庆)1,3 ; Liu Z(刘重)1,3,4; Yang LY(杨丽英)1,3; Gu F(谷丰)1,3
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| 出版日期 | 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 |
| 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.State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, China 2.College of Information Science and Engineering, Northeastern University, Shenyang 110819, 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. |
入库方式： OAI收割
来源：沈阳自动化研究所
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