Title :
Operator based nonlinear vibration control for an aircraft vertical tail with unknown input nonlinearity
Author :
Yuta Katsurayama;Mingcong Deng;Shin Wakitani
Author_Institution :
Department of Electrical and Electronic Engineering, The Graduate School of Engineering, Tokyo University of Agriculture and Technology, Tokyo, Japan
fDate :
7/1/2015 12:00:00 AM
Abstract :
In this paper, operator based robust nonlinear vibration control method for an aircraft vertical tail with piezoelectric actuators is proposed. Firstly, models of a hysteresis nonlinearity of piezoelectric actuators by Plandtl-Ishlinskii model and the plate that is simulated an aircraft vertical tail are introduced. Secondly, with use of operator theory, a control design of the plate that has an effect of input nonlinearities is proposed to stabilize the system. Then, the desired dumping effect of the plate is discussed. Finally, the proposed control design is verified by simulations.
Keywords :
"Piezoelectric actuators","Hysteresis","Mathematical model","Atmospheric modeling","Aircraft","Vibrations"
Conference_Titel :
Society of Instrument and Control Engineers of Japan (SICE), 2015 54th Annual Conference of the
DOI :
10.1109/SICE.2015.7285337
