DocumentCode :
3181128
Title :
Intelligent Rotor Speed Controller for a Mini Autonomous Helicopter
Author :
Xu, Yu ; Li, Ping ; Han, Bo ; Ren, Qinyuan
Author_Institution :
Nat. Lab. of Ind. Control Technol., Zhejiang Univ., Hangzhou
fYear :
2006
fDate :
9-15 Oct. 2006
Firstpage :
2918
Lastpage :
2923
Abstract :
Rotor is the most important component in mini autonomous helicopter. In order to simplify identification and control, it is desirable for mini autonomous helicopter to hold rotor speed constant, since varying rotor speed causes varying aerodynamics. An intelligent rotor speed controller has been developed, which adopts the control algorithms of feed forward and fuzzy tuned PI. The hardware design especially the tachometer design is described in this paper. To improve the performance of PI controller, a fuzzy logic supervisor has been proposed for tuning the gain parameters of PI controller online. The controller is then applied in a mini autonomous helicopter to verify its performance. The experimental results of real flights have shown that the intelligent rotor speed controller is superior in dynamic and steady state performance for its advantages of quick response and good robustness. Numerous flights have also proven its reliability
Keywords :
PI control; feedforward; fuzzy control; helicopters; microrobots; remotely operated vehicles; velocity control; PI control; aerodynamics; feedforward control; fuzzy control; fuzzy logic supervisor; intelligent rotor speed controller; miniautonomous helicopter; tachometer design; Aerodynamics; Algorithm design and analysis; Feeds; Fuzzy control; Fuzzy logic; Hardware; Helicopters; Performance gain; Robust control; Steady-state; feed forward; fuzzy tuned PI; mini autonomous helicopter; tachometer;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Robots and Systems, 2006 IEEE/RSJ International Conference on
Conference_Location :
Beijing
Print_ISBN :
1-4244-0258-1
Electronic_ISBN :
1-4244-0259-X
Type :
conf
DOI :
10.1109/IROS.2006.282144
Filename :
4058838
Link To Document :
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