Evolution Driven Controller Design for Aeroservoelastic Aircraft
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26230%2F13%3APU106419" target="_blank" >RIV/00216305:26230/13:PU106419 - isvavai.cz</a>
Result on the web
<a href="http://arc.aiaa.org/doi/abs/10.2514/6.2013-5153" target="_blank" >http://arc.aiaa.org/doi/abs/10.2514/6.2013-5153</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.2514/6.2013-5153" target="_blank" >10.2514/6.2013-5153</a>
Alternative languages
Result language
angličtina
Original language name
Evolution Driven Controller Design for Aeroservoelastic Aircraft
Original language description
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.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
10201 - Computer sciences, information science, bioinformathics (hardware development to be 2.2, social aspect to be 5.8)
Result continuities
Project
Result was created during the realization of more than one project. More information in the Projects tab.
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2013
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Conference Proceeding Series (GNC/AFM/MST)
ISBN
978-1-62993-153-1
ISSN
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e-ISSN
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Number of pages
17
Pages from-to
1-17
Publisher name
American Institute of Aeronautics and Astronautics
Place of publication
Boston, MA
Event location
Boston, Massachusetts
Event date
Aug 19, 2013
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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