DocumentCode
425663
Title
Robust H2 problem for LPV systems and its application to model-following controller design for aircraft motions
Author
Sato, Masayuki
Author_Institution
Inst. of Space Technol. & Aeronaut., Japan Aerosp. Exploration Agency, Tokyo, Japan
Volume
1
fYear
2004
fDate
2-4 Sept. 2004
Firstpage
442
Abstract
This paper considers the problem of robust static output H2 controller design for linear parameter-varying (LPV) systems using parameter-dependent Lyapunov functions. The proposed method uses an iterative algorithm that has monotonic convergence to an optimal solution. The proposed design method is also applied to a previously proposed model-following controller design to overcome its drawbacks. We design several model-following controllers for lateral/directional motions of an experimental aircraft and demonstrate controller performance by experiments.
Keywords
H∞ control; Lyapunov methods; aircraft control; control system synthesis; convergence; iterative methods; linear systems; motion control; robust control; aircraft motions; iterative algorithm; linear parameter varying system; model following controller design; monotonic convergence; parameter dependent Lyapunov functions; robust H2 problem; static output H2 controller design; Aerodynamics; Aerospace control; Aircraft; Control systems; Design methodology; Iterative algorithms; Lyapunov method; Motion control; Optimal control; Robust control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 2004. Proceedings of the 2004 IEEE International Conference on
Print_ISBN
0-7803-8633-7
Type
conf
DOI
10.1109/CCA.2004.1387251
Filename
1387251
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