Evolution Assisted Flight Control System Design

Result code in 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>

Result on the web

<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>

Result language

angličtina

Original language name

Evolution Assisted Flight Control System Design

Original language description

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.

Czech name

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Czech description

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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)

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)

Publication year

2013

Confidentiality

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

Article name in the collection

Proceedings of 32nd Digital Avionics Systems Conference

ISBN

978-1-4799-1536-1

ISSN

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e-ISSN

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Number of pages

9

Pages from-to

1-9

Publisher name

IEEE Computer Society

Place of publication

Syracuse, NY

Event location

Syracuse, NY

Event date

Oct 6, 2013

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

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