DocumentCode
3074539
Title
Robust stabilization of a helicopter model
Author
Kienitz, Karl Heinz ; Wu, Q.-H. ; Mansour, M.
Author_Institution
Inst. for Autom. Control, Swiss Federal Inst. of Technol., Zurich, Switzerland
fYear
1990
fDate
5-7 Dec 1990
Firstpage
2607
Abstract
A case study in robust control is presented which assesses the availability of two robust stabilization methods for practical purposes. The methods considered accomplish H ∞ robust stabilization and quadratic stabilization, respectively. The system of concern is a helicopter-like laboratory model with two degrees of freedom. A comparison of the systems shows the superiority of the quadratically stabilizing controller. The main reason for this lies in the fact that uncertainty structure is considered in the Lyapunov-based design
Keywords
Lyapunov methods; aircraft control; control system synthesis; helicopters; optimal control; stability; Lyapunov-based design; aircraft control; helicopter model; optimal control; quadratic stabilization; robust control; stability; Automatic control; DC motors; Design methodology; Helicopters; Laboratories; Nonlinear equations; Parameter estimation; Robust control; Robustness; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1990., Proceedings of the 29th IEEE Conference on
Conference_Location
Honolulu, HI
Type
conf
DOI
10.1109/CDC.1990.203343
Filename
203343
Link To Document