Detail publikačního výsledku

Evolution Assisted Flight Control System Design

CHUDÝ, P.; VLK, J.; DITTRICH, P.

Originální název

Evolution Assisted Flight Control System Design

Anglický název

Evolution Assisted Flight Control System Design

Druh

Stať ve sborníku v databázi WoS či Scopus

Originální abstrakt

An evolution driven controller design approach has beenapplied to a rigid body aircraft model of a lightsport aircraft. The model comprises inertial, aerodynamic and flightdynamics related elements with the controller architecture based on ClassicalControl Theory. The evolution driven concept has played a significant role inthe optimization of the proposed controller structure by providing tunedcontroller parameters, which meet the designed fitness function criteriaimposed through the optimization problem formulation. The proposed fitnessfunction combines significant controller stability evaluation conditions into asingle abstraction. The use of a robust optimization framework based on thegenetic algorithms has allowed the suggested form of multi-criteriaoptimization definition. The suitability of the evolutionary optimization hasbeen successfully tested on a model with rigid body aircraft dynamics.Time-domain simulation results have shown the compliance of the tunedcontroller performance with its anticipated behavior.

Anglický abstrakt

An evolution driven controller design approach has beenapplied to a rigid body aircraft model of a lightsport aircraft. The model comprises inertial, aerodynamic and flightdynamics related elements with the controller architecture based on ClassicalControl Theory. The evolution driven concept has played a significant role inthe optimization of the proposed controller structure by providing tunedcontroller parameters, which meet the designed fitness function criteriaimposed through the optimization problem formulation. The proposed fitnessfunction combines significant controller stability evaluation conditions into asingle abstraction. The use of a robust optimization framework based on thegenetic algorithms has allowed the suggested form of multi-criteriaoptimization definition. The suitability of the evolutionary optimization hasbeen successfully tested on a model with rigid body aircraft dynamics.Time-domain simulation results have shown the compliance of the tunedcontroller performance with its anticipated behavior.

Klíčová slova

Evolution, light sport aircraft, framework, time-domain, control, genetic algrithm.

Klíčová slova v angličtině

Evolution, light sport aircraft, framework, time-domain, control, genetic algrithm.

Autoři

CHUDÝ, P.; VLK, J.; DITTRICH, P.

Rok RIV

2014

Vydáno

14.09.2013

Nakladatel

IEEE Computer Society

Místo

Syracuse, NY

ISBN

978-1-4799-1536-1

Kniha

Proceedings of 32nd Digital Avionics Systems Conference

Strany od

1

Strany do

9

Strany počet

9

URL

BibTex

@inproceedings{BUT103566,
  author="Peter {Chudý} and Jan {Vlk} and Petr {Dittrich}",
  title="Evolution Assisted Flight Control System Design",
  booktitle="Proceedings of 32nd Digital Avionics Systems Conference",
  year="2013",
  pages="1--9",
  publisher="IEEE Computer Society",
  address="Syracuse, NY",
  doi="10.1109/DASC.2013.6712641",
  isbn="978-1-4799-1536-1",
  url="http://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=6712641"
}