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

fYear

2013

fDate

25-27 Sept. 2013

Firstpage

335

Lastpage

340

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;

fLanguage

English

Publisher

ieee

Conference_Titel

Advanced Mechatronic Systems (ICAMechS), 2013 International Conference on

Conference_Location

Luoyang

Print_ISBN

978-1-4799-2518-6

Type

conf

DOI

10.1109/ICAMechS.2013.6681804

Filename

6681804