Modeling, Control and Flight Testing for a Saucer Ducted Fan UAV

摘要：

This paper mainly focuses on the dynamic analysis and control system design of the small saucer ducted fan unmanned vehicle. The dynamic of the UAV is analyzed first in this paper and a simulation model is constructed from the forces and moments analysis of the vehicle in the flight node of hovering. After that a robust controller based on H2 H∞ is designed to handle the attitude control problem, and then the simulation results are presented. Finally, the flight testing was completed.

作者: Wang Changhong Li Yuanwei Xi Boqi Guoxing Yi

作者单位: Space Control and Inertial Technology Research Center,Harbin Institute of Technology Harbin 150080,China

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 934-940

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）