DGLR-Publikationsdatenbank - Detailansicht
Titel:
Analysis and Wind Tunnel Tests of Different Control Laws for Active Flutter Suppression
Autor(en):
D. Guan, G. Chen
Zusammenfassung:
Active flutter suppression may be more hopeful to be put into practical application on wing-store configuration. A series of analysis and low speed wind tunnel tests for a wing-store model were conducted and different kinds of control laws were investigated. The first and second control laws are based on the combination of pole assignment and optimal control theory by use of dual optimization procedure and dynamic compensator respectively. The third one was designed by use of aerodynamic energy method. These control laws have been realized in low speed wind tunnel tests and the experimental characteristics of flutter suppression correlate well with the predicted values.
Veranstaltung:
International Forum on Aeroelasticity and Structural Dynamics 1991, Aachen
Medientyp:
Conference Paper
Sprache:
englisch
Format:
21,0 x 29,7 cm, 5 Seiten
Veröffentlicht:
DGLR-Bericht, 1991, 1991-06, International Forum on Aeroelasticity and Structural Dynamics 1991 Proceedings; S.469-473; 1991; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn
Preis:
NA
ISBN:
ISSN:
Kommentar:
Klassifikation:
Stichworte zum Inhalt:
aeroelasticity
Verfügbarkeit:
Bestellbar
Veröffentlicht:
1991
Dieses Dokument ist Teil einer übergeordneten Publikation:
International Forum on Aeroelasticity and Structural Dynamics 1991 Proceedings