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CHUDÝ, P. LEITAO, M. STROSCHER, F. VLK, J.
Originální název
Evolution Driven Controller Design for Aeroservoelastic Aircraft
Typ
článek ve sborníku ve WoS nebo Scopus
Jazyk
angličtina
Originální abstrakt
An evolution driven controller design approach has been appliedto an aeroservoelastic model of a large passenger aircraft. Theaeroservoelastic model comprises structural, aerodynamic and flight dynamicsrelated elements and the chosen controller architecture is based on NonlinearDynamic Inversion. The evolutionary concept has played a significant role inthe optimization of the proposed NDI controller structure by providing tunedcontroller parameters which meet the designed fitness function criteria imposedthrough the optimization problem formulation. The proposed fitness function combinessignificant controller stability evaluation criteria into a single abstraction.The use of a robust optimization framework based on the genetic algorithms has allowedthe suggested form of multi-criteria optimization definition. The suitabilityof the evolutionary optimization has been successfully tested on a set ofexamples, which accounted for rigid body aircraft dynamics as well as for thecase with elastic structural modes. Time-domain simulation results have shownthe compliance of the tuned controller performance to its anticipated behavior.
Klíčová slova
Evolutionary algorithms, Numerical optimization, Controller Design, Aeroservoelastic aircraft, Nonlinear dynamic inversion, Pseudo Control Hedging
Autoři
CHUDÝ, P.; LEITAO, M.; STROSCHER, F.; VLK, J.
Rok RIV
2013
Vydáno
21. 8. 2013
Nakladatel
American Institute of Aeronautics and Astronautics
Místo
Boston, MA
ISBN
978-1-62993-153-1
Kniha
Conference Proceeding Series (GNC/AFM/MST)
Edice
AIAA Modeling and Simulation Technologies (MST) Conference
Strany od
1
Strany do
17
Strany počet
URL
http://arc.aiaa.org/doi/abs/10.2514/6.2013-5153
BibTex
@inproceedings{BUT103559, author="Peter {Chudý} and Miguel {Leitao} and Felix {Stroscher} and Jan {Vlk}", title="Evolution Driven Controller Design for Aeroservoelastic Aircraft", booktitle="Conference Proceeding Series (GNC/AFM/MST)", year="2013", series="AIAA Modeling and Simulation Technologies (MST) Conference", pages="1--17", publisher="American Institute of Aeronautics and Astronautics", address="Boston, MA", doi="10.2514/6.2013-5153", isbn="978-1-62993-153-1", url="http://arc.aiaa.org/doi/abs/10.2514/6.2013-5153" }