Title :
Robust control for uncertain systems with application to helicopter model
Author :
Yoneyama, Jun ; Kikuchi, Yukihisa
Author_Institution :
Dept. of Electron. & Electr. Eng., Aoyama Gakuin Univ., Tokyo, Japan
Abstract :
This paper is concerned with robust stabilization and robust H∞ control of a class of uncertain systems. The class of the systems is continuous-time systems with norm-bounded time-varying parameter uncertainties. We first show relationships between robust H∞ control via linear output feedback and a scaled H∞ control problem and between quadratic stabilization and a standard H∞ control problem for uncertain systems. These implies that a quadratic stabilizing controller for uncertain systems can be designed by solving a standard H∞ controller. Next, the results are applied to a helicopter model. The model is likely to have identification error between the original model and its linear mathematical representation. It is shown that robust controllers designed for uncertain systems work effectively.
Keywords :
H∞ control; aircraft control; control system synthesis; feedback; helicopters; nonlinear dynamical systems; robust control; time-varying systems; uncertain systems; continuous-time systems; helicopter model; identification error; linear mathematical representation; linear output feedback; nonlinear dynamical systems; norm-bounded time-varying parameter uncertainties; quadratic stabilization; quadratic stabilizing controller; robust H∞ control; robust control; robust stabilization; scaled H∞ control problem; uncertain systems; Control systems; Helicopters; Linear feedback control systems; Mathematical model; Nonlinear control systems; Nonlinear dynamical systems; Output feedback; Robust control; Uncertain systems; Uncertainty;
Conference_Titel :
SICE 2002. Proceedings of the 41st SICE Annual Conference
Print_ISBN :
0-7803-7631-5
DOI :
10.1109/SICE.2002.1195351