DocumentCode
1561078
Title
Control System Design for Silicon MEMS-based Micro UAV
Author
Fang Jian Cheng ; Tao Ye ; Sheng Wei
Author_Institution
School of Instrument and Optoelectric Engineering, Beijing University of Aeronautics and Astronautics, Beijing, 100083, China
fYear
2006
Firstpage
2137
Lastpage
2140
Abstract
In this paper, piece-wise PID controller is developed for a class of Micro UAV. In UAV´s fixed-point flight, by applying the designed controller in UAV´s longitudinal and transverse control systems, fixed-attitude stabilized control and tracking control of fixed-height and fixed-destination flight can be effectively realized. The experimental results verifies the stability of pitching and rolling channels. The results show the controller has good performance in restraining unfavorable effects from uncertainty, and dynamic tracking performance is well guaranteed.
Keywords
Control systems; Equations; Linear feedback control systems; Motion control; Optimal control; Silicon; Systems engineering and theory; Three-term control; Unmanned aerial vehicles; Velocity control; Micro; UAV; trajectory tracking;
fLanguage
English
Publisher
ieee
Conference_Titel
Computational Engineering in Systems Applications, IMACS Multiconference on
Conference_Location
Beijing, China
Print_ISBN
7-302-13922-9
Electronic_ISBN
7-900718-14-1
Type
conf
DOI
10.1109/CESA.2006.313479
Filename
4105732
Link To Document