DocumentCode
3041514
Title
Modeling, control and flight testing for a saucer ducted fan UAV
Author
Changhong, Wang ; Yuanwei, Li ; Boqi, Xi ; Guoxing, Yi
Author_Institution
Control Science & Engineering Department, Harbin Institute of Technology, China
fYear
2010
fDate
8-10 June 2010
Firstpage
930
Lastpage
935
Abstract
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.
Keywords
Atmospheric modeling; Bismuth; Facsimile; Iron;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location
Harbin, China
Print_ISBN
978-1-4244-6043-4
Electronic_ISBN
978-1-4244-7505-6
Type
conf
DOI
10.1109/ISSCAA.2010.5633048
Filename
5633048
Link To Document