Modeling and hover control of a dual-rotor tail-sitter unmanned aircraft

Jingyang Zhong, Bifeng Song, Wenqing Yang, Peng Nian

科研成果: 书/报告/会议事项章节会议稿件同行评审

4 引用 (Scopus)

摘要

A tail-sitter unmanned aircraft is capable of transition between horizontal and vertical flight. This paper highlights topics of interest to developing a more accurate model to make the simulation results more reasonable. The modeling processes are presented in details. Aerodynamics of this unmanned aircraft is obtained by wind tunnel tests associated with aerodynamic estimation software. Characters of propeller slipstream are analyzed and the mathematical relationships among slipstream velocity, propeller speed, radial location and axial location of propeller plane are deduced from the experiment data. Besides, separate consideration of the propeller slipstream on wings and control surfaces gives better estimations on the dynamic pressure. Models of actuators and motors are also obtained through some tests to make the results reliable. Furthermore, a simple controller is designed to implement the hover attitude control.

源语言英语
主期刊名Intelligent Robotics and Applications - 10th International Conference, ICIRA 2017, Proceedings
编辑Honghai Liu, YongAn Huang, Hao Wu, Zhouping Yin
出版商Springer Verlag
589-601
页数13
ISBN(印刷版)9783319652979
DOI
出版状态已出版 - 2017
活动10th International Conference on Intelligent Robotics and Applications, ICIRA 2017 - Wuhan, 中国
期限: 16 8月 201718 8月 2017

出版系列

姓名Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)
10464 LNAI
ISSN(印刷版)0302-9743
ISSN(电子版)1611-3349

会议

会议10th International Conference on Intelligent Robotics and Applications, ICIRA 2017
国家/地区中国
Wuhan
时期16/08/1718/08/17

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