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Modeling and LPV flight control of the Canard Rotor/ Wing unmanned aerial vehicle

  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

The concept, known as the Canard Rotor/Wing (CRW) unmanned aerial vehicle (UAV) combines the hover flight characteristic of a helicopter with high subsonic cruise of a fixed-wing aircraft. The longitudinal flight dynamic model of CRW was developed, and the trim result was derived in the full flight envelope. The linear model of CRW was derived by the Jacobian linear method, and it was nonlinearly dependent on the time-varying flight speed and altitude. The tensor-product (TP) model transformation was adopted to transform the model to a convex polytopic model form. Hence, a linear parameter-varying (LPV) synthesis method was used to design the flight control system of CRW in the rotary mode. The simulation results show that the desired performance objectives are achieved in the rotary flight stage.

源语言英语
主期刊名2011 2nd International Conference on Artificial Intelligence, Management Science and Electronic Commerce, AIMSEC 2011 - Proceedings
2187-2191
页数5
DOI
出版状态已出版 - 2011
活动2011 2nd International Conference on Artificial Intelligence, Management Science and Electronic Commerce, AIMSEC 2011 - Zhengzhou, 中国
期限: 8 8月 201110 8月 2011

出版系列

姓名2011 2nd International Conference on Artificial Intelligence, Management Science and Electronic Commerce, AIMSEC 2011 - Proceedings

会议

会议2011 2nd International Conference on Artificial Intelligence, Management Science and Electronic Commerce, AIMSEC 2011
国家/地区中国
Zhengzhou
时期8/08/1110/08/11

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