Aeroelastic wing section control via relaxed tensor product model transformation framework

Péter Baranyi, Béla Takarics

Research output: Contribution to journalArticle

16 Citations (Scopus)

Abstract

A study was conducted to demonstrate aeroelastic wing section control via relaxed tensor product model transformation framework. The investigations focused on the three-degree-of-freedom (3-DOF) nonlinear aeroelastic test apparatus (NATA) model. The study also revisited the parallel distributed compensation (PDC) framework-based control solution of the 3-DOF NATA model in the case where the model was extended to incorporate friction. It presented a new general theoretical control design framework based on tensor product (TP) model transformation. The proposed framework was capable of a significant complexity reduction of quasi-linear parameter-varying (QLPV) models, including numerical and theoretical for linear matrix inequality (LMI)-based control design. The proposed control design framework was applied for active stabilization of the 3-DOF aeroelastic wing section as an extension of the design method.

Original languageEnglish
Pages (from-to)1671-1677
Number of pages7
JournalJournal of Guidance, Control, and Dynamics
Volume37
Issue number5
DOIs
Publication statusPublished - Sep 1 2014

ASJC Scopus subject areas

  • Control and Systems Engineering
  • Aerospace Engineering
  • Space and Planetary Science
  • Electrical and Electronic Engineering
  • Applied Mathematics

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