Conference paper

CHUDÝ Peter, LEITAO Miguel, STROSCHER Felix and VLK Jan. Evolution Driven Controller Design for Aeroservoelastic Aircraft. In: Conference Proceeding Series (GNC/AFM/MST). 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
Publication language:english
Original title:Evolution Driven Controller Design for Aeroservoelastic Aircraft
Title (cs):Evoluční návrh regulátoru pro aeroservoelastický letoun
Pages:1-17
Proceedings:Conference Proceeding Series (GNC/AFM/MST)
Conference:AIAA Modeling and Simulation Technologies Conference 2013
Series:AIAA Modeling and Simulation Technologies (MST) Conference
Place:Boston, MA, US
Year:2013
URL:http://arc.aiaa.org/doi/abs/10.2514/6.2013-5153
ISBN:978-1-62993-153-1
Publisher:American Institute of Aeronautics and Astronautics
Keywords
Evolutionary algorithms, Numerical optimization, Controller Design, Aeroservoelastic aircraft, Nonlinear dynamic inversion, Pseudo Control Hedging
Annotation
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.
BibTeX:
@INPROCEEDINGS{
   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},
   language = {english},
   url = {http://www.fit.vutbr.cz/research/view_pub.php?id=10440}
}

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