TY - GEN
T1 - Modeling, control and flight testing for a saucer ducted fan UAV
AU - Wang, Changhong
AU - Li, Yuanwei
AU - Xi, Boqi
AU - Yi, Guoxing
PY - 2010
Y1 - 2010
N2 - 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.
AB - 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.
UR - https://www.scopus.com/pages/publications/79952130177
U2 - 10.1109/ISSCAA.2010.5633048
DO - 10.1109/ISSCAA.2010.5633048
M3 - 会议稿件
AN - SCOPUS:79952130177
SN - 9781424460441
T3 - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
SP - 930
EP - 935
BT - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
T2 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010
Y2 - 8 June 2010 through 10 June 2010
ER -