DGLR-Publikationsdatenbank - Detailansicht
Titel:
Helicopter Sling Load Positioning
Autor(en):
H. Brenner
Zusammenfassung:
The paper at hand addresses the precise positioning control of helicopter sling loads. Due to a significant decrease in handling qualities caused by the external load, the manual load positioning can be hindered. By means of linear quadratic optimal output regulation, the helicopter position as well as the load sway are controlled in an integrated approach. The position control is part of an existing AFCS, which guarantees for the basic helicopter stability. The controllers are developed and tested on the basis of a comprehensive system simulation.
Veranstaltung:
35th European Rotorcraft Forum 2009,
Medientyp:
Conference Paper
Sprache:
englisch
Format:
21,0 x 29,7 cm, 15 Seiten
Veröffentlicht:
DGLR-Bericht, 2009, 2009-03, 35th European Rotorcraft Forum 2009 - Conference Proceedings; S.1-15; 2009; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn
Preis:
NA
ISBN:
ISSN:
Kommentar:
in getr. Zählung;
Klassifikation:
Stichworte zum Inhalt:
helicopters, sling loads
Verfügbarkeit:
Bestellbar
Veröffentlicht:
2009
Dieses Dokument ist Teil einer übergeordneten Publikation:
35th European Rotorcraft Forum 2009 - Conference Proceedings