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Modeling and hover control of a novel unmanned coaxial rotor/ducted-fan helicopter

  • Hongqiang Wang*
  • , Daobo Wang
  • , Xinwen Niu
  • , Haibin Duan
  • *此作品的通讯作者
  • Nanjing University of Aeronautics and Astronautics

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

In this paper, we consider the problem of controlling a novel rotor/ducted-fan helicopter. After some qualitative introduction on the new arrangement helicopter and its flight behavior, we establish the nonlinear model of the helicopter using a top-down principle based on Newton-Euler equations. Then the linearized model for the helicopter in hover is derived in order to perform analysis and controller design. By observing the helicopter response to control inputs, we found that the coaxial ducted-fan has very different crossed-coupling characteristics in comparison with conventional helicopter, that is, the strong couplings between pitch and roll as well as vertical to yaw. This is mainly caused by the special coaxial and axial symmetric arrangement. Finally, a hover controller is designed for the helicopter by means of robust H-infinity control methodology. The selection of the weighting matrices in the process of H-infinity design is also discussed. Simulation results demonstrate the validity of the analysis and control design.

源语言英语
主期刊名Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2007
1768-1773
页数6
DOI
出版状态已出版 - 2007
活动2007 IEEE International Conference on Automation and Logistics, ICAL 2007 - Jinan, 中国
期限: 18 8月 200721 8月 2007

出版系列

姓名Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2007

会议

会议2007 IEEE International Conference on Automation and Logistics, ICAL 2007
国家/地区中国
Jinan
时期18/08/0721/08/07

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