DocumentCode
3136444
Title
MIMO controller design for decoupling aircraft lateral dynamics
Author
Keviczky, L. ; Bányász, Cs
Author_Institution
Dept. of Autom. & Inf., Budapest Univ. of Technol. & Econ., Budapest, Hungary
fYear
2011
fDate
19-21 Dec. 2011
Firstpage
1079
Lastpage
1084
Abstract
The principal lateral motion of an aircraft is described by a minimum of fourth order coupled state variable model. It is interesting to investigate how a decoupling controller can be designed. The Youla-parametrization is a simple method to design controllers. The KB-parametrization is a successful extension of this method for two-degree-of-freedom (2DOF) systems. The paper extends this methodology for multivariable case and applies to the decoupling lateral control.
Keywords
MIMO systems; aircraft; control system synthesis; motion control; KB parametrization; MIMO controller design; Youla parametrizution; aircraft lateral dynamics decoupling; decoupling controller; fourth order coupled state variable model; multivariable case; principal lateral motion; two-degree-of-freedom systems; Computational modeling; MIMO; Mathematical model; Polynomials; Regulators;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Automation (ICCA), 2011 9th IEEE International Conference on
Conference_Location
Santiago
ISSN
1948-3449
Print_ISBN
978-1-4577-1475-7
Type
conf
DOI
10.1109/ICCA.2011.6137900
Filename
6137900
Link To Document