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Helicopter Sling Load Pendulum Damping

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

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Abstract

Helicopters carrying sling loads suffer a decrease in handling qualities. In addition, the pilot control task is expanded by controlling the sling load. Both factors contribute to a significant increase in pilot workload, which can lead to a reduction in flight safety. In order to support sling load operations, the control of the load - damping and stabilization of the load pendulum swing - can be automatized by means of feedback of the load dynamic. The load pendulum controllers are integrated into an existing AFCS, featuring limitations in actuator rate and saturation. Based on a comprehensive simulation of the overall helicopter-slings-load system, an algorithm for the automatic determination of optimal feedback controllers has been developed. Selected controllers are tested for the potential of increasing the load pendulum damping and for the robustness under parameter variations.

Item URL in elib:https://elib.dlr.de/60240/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Helicopter Sling Load Pendulum Damping
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Brenner, HannoUNSPECIFIEDUNSPECIFIED
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 SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:helicopter, sling load, automatic 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 15:00
Last Modified:21 Oct 2009 15:00

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