DocumentCode :
3158383
Title :
Control System Design for Silicon MEMS-based Micro UAV
Author :
Cheng, Fang Jian ; Ye, Tao ; Wei, Sheng
Author_Institution :
Sch. of Instalment & Optoelectric Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing
Volume :
2
fYear :
2006
fDate :
4-6 Oct. 2006
Firstpage :
2137
Lastpage :
2140
Abstract :
In this paper, piecewise 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 :
aerospace robotics; attitude control; control system synthesis; microrobots; mobile robots; remotely operated vehicles; stability; telerobotics; three-term control; tracking; control system design; fixed-attitude stabilized control; fixed-point flight control; longitudinal control system; piecewise PID controller; silicon MEMS-based microUAV; tracking control; transverse control system; 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
Print_ISBN :
7-302-13922-9
Electronic_ISBN :
7-900718-14-1
Type :
conf
DOI :
10.1109/CESA.2006.4281991
Filename :
4281991
Link To Document :
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