Aeroelastic wing section control via relaxed tensor product model transformation framework

Baranyi, Péter Zoltán and Takarics, Béla (2014) Aeroelastic wing section control via relaxed tensor product model transformation framework. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 37 (5). pp. 1671-1677. ISSN 0731-5090 10.2514/1.G000080

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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.

Item Type: Article
Uncontrolled Keywords: Tensors; Three-degree-of-freedom (3-DOF); Test apparatus; Tensor product models; Parallel distributed compensation; Control solutions; complexity reduction; Aeroelastic wings; Active stabilization; Product design; Linear matrix inequalities; Feedback control; DESIGN; aeroelasticity
Subjects: Q Science > QA Mathematics and Computer Science > QA75 Electronic computers. Computer science / számítástechnika, számítógéptudomány
Divisions: 3D Internet-based Control and Communications Laboratory
SWORD Depositor: MTMT Injector
Depositing User: MTMT Injector
Date Deposited: 03 Feb 2015 12:26
Last Modified: 03 Feb 2015 12:26
URI: http://eprints.sztaki.hu/id/eprint/8162

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