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The stability analysis of quadrotor unmanned aerial vechicles

  • Yun Ping Liu*
  • , Xian Ying Li
  • , Tian Miao Wang
  • , Yong Hong Zhang
  • , Ping Mei
  • *此作品的通讯作者
  • Nanjing University of Information Science & Technology
  • 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 problems of dynamic stability of the quadrotor Unmanned Aerial Vehicles (UAV), such as: cornering, wear, and explosion of oar take place due to the aerodynamic force and gyroscopic effect during takeoff and landing process; the vibration; reduction of instruction tracking accuracy; and out of control are prone to take place due to the influence of atmospheric turbulence and motion coupling during yawing. However, the optimized structural parameters of the aircraft is very important for improving the stability of the motion control and the energy saving. Therefore, the relationship of quantification between structural parameter of quadrotor UAV and dynamic stability is built with the method of Lyapunov exponent starting from structure design of mechanical, which guides the mechanical structural design and provides important basis for optimizing the control system. This relationship lays a basic foundation for enhancing the reliability and stability for the flight mission. Compared with the direct method of Lyapunov, the method of Lyapunov exponent is easier to build, and the calculation process is simpler.

源语言英语
主期刊名Wearable Sensors and Robots - Proceedings of International Conference on Wearable Sensors and Robots 2015
编辑G.S. Virk, Canjun Yang, Huayong Yang
出版商Springer Verlag
383-394
页数12
ISBN(印刷版)9789811024030
DOI
出版状态已出版 - 2017
活动International Conference on Wearable Sensors and Robots, ICWSR 2015 - Hangzhou, 中国
期限: 16 10月 201518 10月 2015

出版系列

姓名Lecture Notes in Electrical Engineering
399
ISSN(印刷版)1876-1100
ISSN(电子版)1876-1119

会议

会议International Conference on Wearable Sensors and Robots, ICWSR 2015
国家/地区中国
Hangzhou
时期16/10/1518/10/15

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