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Helicopter Sling Load Positioning

Brenner, Hanno (2009) Helicopter Sling Load Positioning. In: Proceedings of the 35th European Rotorcraft Forum. European Rotorcraft Forum, 22.-25. Sep. 2009, Hamburg.

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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.

Item URL in elib:https://elib.dlr.de/60241/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Helicopter Sling Load Positioning
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Date:23 September 2009
Journal or Publication Title:Proceedings of the 35th European Rotorcraft Forum
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:helicopter, sling load, position control, linear quadratic optimal output control
Event Title:European Rotorcraft Forum
Event Location:Hamburg
Event Type:international Conference
Event Dates:22.-25. Sep. 2009
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft (old)
DLR - Research area:Aeronautics
DLR - Program:L DT - Drehflüglertechnologien
DLR - Research theme (Project):L - The Smart Rotorcraft (old)
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Deposited By: Brenner, Hanno
Deposited On:21 Oct 2009 15:01
Last Modified:21 Oct 2009 15:01

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