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 :
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