Publication Details

Evolution Driven Controller Design for Aeroservoelastic Aircraft

CHUDÝ Peter, LEITAO Miguel, STROSCHER Felix and VLK Jan. Evolution Driven Controller Design for Aeroservoelastic Aircraft. In: Conference Proceeding Series (GNC/AFM/MST). AIAA Modeling and Simulation Technologies (MST) Conference. Boston, MA: American Institute of Aeronautics and Astronautics, 2013, pp. 1-17. ISBN 978-1-62993-153-1. Available from: http://arc.aiaa.org/doi/abs/10.2514/6.2013-5153
Czech title
Evoluční návrh regulátoru pro aeroservoelastický letoun
Type
conference paper
Language
english
Authors
Chudý Peter, doc. Ing., Ph.D. MBA (DCGM FIT BUT)
Leitao Miguel, M.Sc. (TUM)
Stroscher Felix, Dipl.-Ing. (TUM)
Vlk Jan, Ing., Ph.D. (DCGM FIT BUT)
URL
Keywords

Evolutionary algorithms, Numerical optimization, Controller Design, Aeroservoelastic aircraft, Nonlinear dynamic inversion, Pseudo Control Hedging

Abstract

An evolution driven controller design approach has been applied to an aeroservoelastic model of a large passenger aircraft. The aeroservoelastic model comprises structural, aerodynamic and flight dynamics related elements and the chosen controller architecture is based on Nonlinear Dynamic Inversion. The evolutionary concept has played a significant role in the optimization of the proposed NDI controller structure by providing tuned controller parameters which meet the designed fitness function criteria imposed through the optimization problem formulation. The proposed fitness function combines significant controller stability evaluation criteria into a single abstraction. The use of a robust optimization framework based on the genetic algorithms has allowed the suggested form of multi-criteria optimization definition. The suitability of the evolutionary optimization has been successfully tested on a set of examples, which accounted for rigid body aircraft dynamics as well as for the case with elastic structural modes. Time-domain simulation results have shown the compliance of the tuned controller performance to its anticipated behavior.

Published
2013
Pages
1-17
Proceedings
Conference Proceeding Series (GNC/AFM/MST)
Series
AIAA Modeling and Simulation Technologies (MST) Conference
Conference
AIAA Modeling and Simulation Technologies Conference 2013, Boston, Massachusetts, US
ISBN
978-1-62993-153-1
Publisher
American Institute of Aeronautics and Astronautics
Place
Boston, MA, US
DOI
EID Scopus
BibTeX
@INPROCEEDINGS{FITPUB10440,
   author = "Peter Chud\'{y} and Miguel Leitao and Felix Stroscher and Jan Vlk",
   title = "Evolution Driven Controller Design for Aeroservoelastic Aircraft",
   pages = "1--17",
   booktitle = "Conference Proceeding Series (GNC/AFM/MST)",
   series = "AIAA Modeling and Simulation Technologies (MST) Conference",
   year = 2013,
   location = "Boston, MA, US",
   publisher = "American Institute of Aeronautics and Astronautics",
   ISBN = "978-1-62993-153-1",
   doi = "10.2514/6.2013-5153",
   language = "english",
   url = "https://www.fit.vut.cz/research/publication/10440"
}
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