Title :
Application of H∞ control to a vibration system using air jet propulsion
Author :
Ichihara, Hiroyuki ; Abe, Naoto ; Kanoh, Hideaki
Author_Institution :
Dept. of Precision Eng., Meiji Univ., Kanagawa, Japan
Abstract :
This paper deals with a vibration control using air jet propulsion. To study its effect, a two links pendulum with a pair of air jet actuators is used as control object. The purpose of the control design is to reject disturbances. We use a simple one link pendulum as a design model. By using identification result of an unmodeled dynamics, we design an H∞ controller to suppress its vibration. In the experiment, we show the effect of air jet propulsion and robust control
Keywords :
H∞ control; actuators; control system synthesis; dynamics; identification; pendulums; pneumatic control equipment; robust control; vibration control; H∞ control; air jet actuators; air jet propulsion; dynamics; identification; pendulum; robust control; vibration control; Actuators; Control design; Control systems; Propulsion; Pulse width modulation; Resonance; Robust control; Springs; Uncertainty; Vibration control;
Conference_Titel :
Control Applications, 1998. Proceedings of the 1998 IEEE International Conference on
Conference_Location :
Trieste
Print_ISBN :
0-7803-4104-X
DOI :
10.1109/CCA.1998.728545
