Robust control design for the FLEXOP demonstrator aircraft via tensor product models

Author:

Takarics Béla12ORCID,Vanek Bálint1ORCID

Affiliation:

1. Systems and Control Lab Institute for Computer Science and Control Budapest Hungary

2. Department of Control for Transportation and Vehicle Systems Budapest University of Technology and Economics Budapest Hungary

Funder

European Commission

Magyar Tudományos Akadémia

Nemzeti Kutatási, Fejlesztési és Innovaciós Alap

Publisher

Wiley

Subject

Control and Systems Engineering

Reference40 articles.

1. PAAW Performance adaptive aeroelastic wing program. Supported by NASA NRA “Lightweight Adaptive Aeroelastic Wing for Enhanced Perfromace Across the Flight Envelope” 2014–2019.

2. FLEXOP Flutter Free FLight Envelope eXpansion for ecOnomical Performance improvement (FLEXOP). H2020 Project ID: 636307 2015‐2018.

3. FliPASED Flight Phase Adaptive Aero‐Servo‐Elastic Aircraft Design Methods (FliPASED). H2020 Project ID: 815058 2019‐2022.

4. Flight control design for a highly flexible flutter demonstrator

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