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Design and experimental study of a new flapping wing rotor micro aerial vehicle

  • Beihang UAS Technology Co. Ltd
  • 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

A new flapping wing rotor micro aerial vehicle named Rotorbee and relevant experimental study are presented in this paper. The flapping rotary mechanism, the transmission mechanism, and the wings were designed for this flapping wing rotor vehicle. The fabrication methods and materials were chosen to assemble Rotorbee. The lift tests under different structural parameters, which include flapping frequency, wing length, initial angle of attack, and rod length of structure, were carried out, resulting in a relatively optimal structure. Take off of the first powered flapping wing rotor micro aerial vehicle was eventually achieved due to innovative design, optimal structure, and proper selection of materials and fabrication methods.

源语言英语
主期刊名Proceedings of 2017 IEEE International Conference on Unmanned Systems, ICUS 2017
编辑Xin Xu
出版商Institute of Electrical and Electronics Engineers Inc.
页29-33
页数5
ISBN(电子版)9781538631065
DOI
出版状态已出版 - 2 7月 2017
活动2017 IEEE International Conference on Unmanned Systems, ICUS 2017 - Beijing, 中国
期限: 27 10月 2017 → 29 10月 2017

丛书

姓名Proceedings of 2017 IEEE International Conference on Unmanned Systems, ICUS 2017
卷2018-January

会议

会议2017 IEEE International Conference on Unmanned Systems, ICUS 2017
国家/地区中国
市Beijing
时期27/10/17 → 29/10/17

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