Title :
Experimental study of nonlinear vibration control for vertical tail with considering low order mode
Author :
Katsurayama, Yuta ; Changan Jiang ; Mingcong Deng
Author_Institution :
Grad. Sch. of Eng., Tokyo Univ. of Agric. & Technol., Koganei, Japan
Abstract :
In this paper, an operator based robust nonlinear vibration control method for an aircraft vertical tail with piezoelectric actuators is proposed. Firstly, experimental devices, the model of the tail and a nonlinear property of hysteresis by Prandtl-Ishlinskii (PI) model are introduced. Secondly, using lower order mode only, the operator based robust nonlinear control design for the tail is designed and the desired performance of tracking is discussed. Finally, the effectiveness of the proposed control scheme is confirmed by experimental results.
Keywords :
PI control; aircraft; control system synthesis; nonlinear control systems; piezoelectric actuators; robust control; vibration control; PI model; Prandtl-Ishlinskii model; aircraft vertical tail; experimental study; low order mode; nonlinear property; piezoelectric actuators; robust nonlinear control design; robust nonlinear vibration control method; Actuators; Aerospace control; Aircraft; Density functional theory; Heating; finite element method; operator theory; piezoelectric actuator; robust nonlinear controller; vertical tail; vibration;
Conference_Titel :
Advanced Mechatronic Systems (ICAMechS), 2013 International Conference on
Conference_Location :
Luoyang
Print_ISBN :
978-1-4799-2518-6
DOI :
10.1109/ICAMechS.2013.6681804
