Evolution Assisted Flight Control System Design

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26230%2F13%3APU106426" target="_blank" >RIV/00216305:26230/13:PU106426 - isvavai.cz</a>

Výsledek na webu

<a href="http://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=6712641" target="_blank" >http://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=6712641</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1109/DASC.2013.6712641" target="_blank" >10.1109/DASC.2013.6712641</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Evolution Assisted Flight Control System Design

Popis výsledku v původním jazyce

An evolution driven controller design approach has been applied to a rigid body aircraft model of a light sport aircraft. The model comprises inertial, aerodynamic and flight dynamics related elements with the controller architecture based on Classical Control Theory. The evolution driven concept has played a significant role in the optimization of the proposed 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 conditions 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 model with rigid body aircraft dynamics. Time-domain simulation results have shown the compliance of the tuned controller performance with its anticipated behavior.

Název v anglickém jazyce

Evolution Assisted Flight Control System Design

Popis výsledku anglicky

An evolution driven controller design approach has been applied to a rigid body aircraft model of a light sport aircraft. The model comprises inertial, aerodynamic and flight dynamics related elements with the controller architecture based on Classical Control Theory. The evolution driven concept has played a significant role in the optimization of the proposed 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 conditions 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 model with rigid body aircraft dynamics. Time-domain simulation results have shown the compliance of the tuned controller performance with its anticipated behavior.

Druh

D - Stať ve sborníku

CEP obor

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OECD FORD obor

10201 - Computer sciences, information science, bioinformathics (hardware development to be 2.2, social aspect to be 5.8)

Projekt

Výsledek vznikl pri realizaci vícero projektů. Více informací v záložce Projekty.

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2013

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

Proceedings of 32nd Digital Avionics Systems Conference

ISBN

978-1-4799-1536-1

ISSN

—

e-ISSN

—

Počet stran výsledku

9

Strana od-do

1-9

Název nakladatele

IEEE Computer Society

Místo vydání

Syracuse, NY

Místo konání akce

Syracuse, NY

Datum konání akce

6. 10. 2013

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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