Tensor-product model-based control of two-dimensional aeroelastic system

Research output: Contribution to journalArticle

70 Citations (Scopus)

Abstract

Use of a recently introduced numerical robust-control design method to stabilize aeroelastic systems according to different control specifications is studied. This numerical design is based on the tensor-product model transformation and the parallel-distributed-compensation design framework. An alternative description of aeroelastic models is also proposed as a gateway to various recent linear-matrix-inequality-based control theories. This study is conducted through an example that focuses attention on the state-variable-feedback controller design to the prototypical aeroelastic wing section with structural nonlinearity. This type of model has been traditionally used for the theoretical as well as experimental analysis of two-dimensional aeroelastic behavior and exhibits limit-cycle oscillation without control effort. Numerical simulations to provide empirical validation of the resulting controllers are presented. Comparison to former alternative control solutions is also presented.

Original languageEnglish
Pages (from-to)391-400
Number of pages10
JournalJournal of Guidance, Control, and Dynamics
Volume29
Issue number2
DOIs
Publication statusPublished - Mar 2006

Fingerprint

Product Model
Model-based Control
Two-dimensional Systems
Tensor Product
Tensors
tensors
products
Numerical Control
controllers
Robust Design
Alternatives
Gateway
Model Transformation
Experimental Analysis
numerical control
design method
Robust Control
Control Theory
Control Design
Controller Design

ASJC Scopus subject areas

  • Aerospace Engineering
  • Instrumentation

Cite this

Tensor-product model-based control of two-dimensional aeroelastic system. / Baranyi, P.

In: Journal of Guidance, Control, and Dynamics, Vol. 29, No. 2, 03.2006, p. 391-400.

Research output: Contribution to journalArticle

@article{aef86700d9c142e9aa49ab24d4124550,
title = "Tensor-product model-based control of two-dimensional aeroelastic system",
abstract = "Use of a recently introduced numerical robust-control design method to stabilize aeroelastic systems according to different control specifications is studied. This numerical design is based on the tensor-product model transformation and the parallel-distributed-compensation design framework. An alternative description of aeroelastic models is also proposed as a gateway to various recent linear-matrix-inequality-based control theories. This study is conducted through an example that focuses attention on the state-variable-feedback controller design to the prototypical aeroelastic wing section with structural nonlinearity. This type of model has been traditionally used for the theoretical as well as experimental analysis of two-dimensional aeroelastic behavior and exhibits limit-cycle oscillation without control effort. Numerical simulations to provide empirical validation of the resulting controllers are presented. Comparison to former alternative control solutions is also presented.",
author = "P. Baranyi",
year = "2006",
month = "3",
doi = "10.2514/1.9462",
language = "English",
volume = "29",
pages = "391--400",
journal = "Journal of Guidance, Control, and Dynamics",
issn = "0731-5090",
publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",
number = "2",

}

TY - JOUR

T1 - Tensor-product model-based control of two-dimensional aeroelastic system

AU - Baranyi, P.

PY - 2006/3

Y1 - 2006/3

N2 - Use of a recently introduced numerical robust-control design method to stabilize aeroelastic systems according to different control specifications is studied. This numerical design is based on the tensor-product model transformation and the parallel-distributed-compensation design framework. An alternative description of aeroelastic models is also proposed as a gateway to various recent linear-matrix-inequality-based control theories. This study is conducted through an example that focuses attention on the state-variable-feedback controller design to the prototypical aeroelastic wing section with structural nonlinearity. This type of model has been traditionally used for the theoretical as well as experimental analysis of two-dimensional aeroelastic behavior and exhibits limit-cycle oscillation without control effort. Numerical simulations to provide empirical validation of the resulting controllers are presented. Comparison to former alternative control solutions is also presented.

AB - Use of a recently introduced numerical robust-control design method to stabilize aeroelastic systems according to different control specifications is studied. This numerical design is based on the tensor-product model transformation and the parallel-distributed-compensation design framework. An alternative description of aeroelastic models is also proposed as a gateway to various recent linear-matrix-inequality-based control theories. This study is conducted through an example that focuses attention on the state-variable-feedback controller design to the prototypical aeroelastic wing section with structural nonlinearity. This type of model has been traditionally used for the theoretical as well as experimental analysis of two-dimensional aeroelastic behavior and exhibits limit-cycle oscillation without control effort. Numerical simulations to provide empirical validation of the resulting controllers are presented. Comparison to former alternative control solutions is also presented.

UR - http://www.scopus.com/inward/record.url?scp=33645571607&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=33645571607&partnerID=8YFLogxK

U2 - 10.2514/1.9462

DO - 10.2514/1.9462

M3 - Article

AN - SCOPUS:33645571607

VL - 29

SP - 391

EP - 400

JO - Journal of Guidance, Control, and Dynamics

JF - Journal of Guidance, Control, and Dynamics

SN - 0731-5090

IS - 2

ER -