Vorträge und Posterpräsentationen (mit Tagungsband-Eintrag):
A. Schirrer, C. Westermayer, M. Hemedi, M. Kozek:
"Robust H-infinity Control Design Parameter Optimization via Genetic Algorithm for Lateral Control of a BWB type Aircraft";
Vortrag: IFAC Workshop on Intelligent Control Systems WICS2010,
Sinaia, Romania;
29.09.2010
- 02.10.2010; in: "Proceedings of the WICS 2010",
IFAC PapersOnline,
(2010),
Paper-Nr. W-10-014,
7 S.
Kurzfassung englisch:
This work presents a comprehensive, optimization-based robust control design approach: utilizing DK-iteration control synthesis and closed-loop evaluation via goal attainment, a genetic algorithm optimizes this design-and-validation process in its free design parameters. This method is applied to a lateral flight control design task for a flexible, large Blended Wing Body (BWB) aircraft configuration. Control goals include time-domain rigid-body response specifications and loads alleviation objectives. First optimization results yield a robust controller that, although not fulfilling all posed goals yet, strongly reduces structure loads compared to an initial design.
Schlagworte:
genetic algorithm, robust control, aerospace application
Zugeordnete Projekte:
Projektleitung Martin Kozek:
Aktive Regelung für ein flexibles 2020 Flugzeug
Erstellt aus der Publikationsdatenbank der Technischen Universität Wien.