中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Controller Design and Flight Experiments for the Dual Tilt Rotor Unmanned Aerial Vehicle in Helicopter Mode

文献类型:会议论文

作者Zheng RJ(郑锐剑)1,3,4; Gu F(谷丰)3,4; Liu Z(刘重)2,3,4; Zhou H(周浩3,4; He YQ(何玉庆)3,4
出版日期2020
会议日期SEP 01-04, 2020
会议地点Athens, GREECE
页码845-853
英文摘要Vertical take-off and landing (VTOL) are the important flying stage of tilt rotor unmanned aerial vehicles (TR-UAV) in helicopter mode. Therefore, the performance of the controller for the helicopter mode will directly impact the safety of DTR-UAV during VTOL stage. To solve this problem, a passivity theory based controller for helicopter mode of dual tilt rotor UAV (DTR-UAV) is proposed and the stability of the method is proved in this work. In the first, the system model of dual tilt rotor is built and divided into longitudinal and lateral dynamic model. Then based on the passivity theory, the robust controller is designed and proved. Finally and more importantly, a dual tilt rotor experiment platform is designed and implemented to verify the feasibility and validity of the proposed method. The results of simulation and experiment show the good performance of the proposed controller.
源文献作者IEEE, IEEE CSS, IEEE Robot & Automat Soc, MCA, ICUAS Assoc, Univ Denver, Univ Denver, Daniel Felix Ritchie Sch Engn & Comp Sci, Tech Univ Crete, Sch Prod Engn & Management, Democritus Univ Thrace, NYU Abu Dhabi, Aristotle Univ Thessaloniki, Dept Mech Engn, Lab Fluid Mech & Trubomachinery, ALTUS, DRONE NODES, Journal Unmanned Vehicle Syst
产权排序1
会议录2020 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS'20)
会议录出版者IEEE
会议录出版地New York
语种英语
ISSN号2373-6720
ISBN号978-1-7281-4278-4
WOS记录号WOS:000612041300112
源URL[http://ir.sia.cn/handle/173321/28319]  
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.University of Chinese Academy of Sciences, Beijing 100049, China
3.Institutes for Robotics and Intelligent Manufacturing, Chinese Academy of Sciences, Shenyang 110169, China
4.State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110819, China
推荐引用方式
GB/T 7714
Zheng RJ,Gu F,Liu Z,et al. Controller Design and Flight Experiments for the Dual Tilt Rotor Unmanned Aerial Vehicle in Helicopter Mode[C]. 见:. Athens, GREECE. SEP 01-04, 2020.

入库方式: OAI收割

来源:沈阳自动化研究所

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