Modeling of Generic Slung Load System

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49 Citationer (Scopus)
13 Downloads (Pure)

Resumé

Udgivelsesdato: MAR-APR
OriginalsprogEngelsk
TidsskriftJournal of Guidance, Control, and Dynamics
Vol/bind32
Udgave nummer2
Sider (fra-til)573-585
ISSN0731-5090
DOI
StatusUdgivet - 2009

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Slings
helicopters
Helicopter
Modeling
Helicopters
modeling
pilot training
lifts
Model
aerodynamics
Aerodynamics
Gauss
simulation
Intuitive
stabilization
Simulation
Stabilization
flight
wire
Wire

Emneord

  • Model
  • Helikopter
  • Slung load

Citer dette

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title = "Modeling of Generic Slung Load System",
abstract = "This paper presents the result of the modelling and verification of a generic slung load system using a small-scale helicopter. The model is intended for use in simulation, pilot training, estimation, and control. The model is derived using a redundant coordinate formulation based on Gauss' Principle of Least Constraint using the Udwadia-Kalaba equation and can be used to model all body to body slung load suspension types. The model provides intuitive and easy-to-use means of modelling and simulating different slung load suspension types. It includes detection of, and response to, wire slackening and tightening as well as aerodynamic coupling between the helicopter and the load. Furthermore, it is shown how the model can be easily used for multi-lift systems either with multiple helicopters or multiple loads. A numerical stabilisation algorithm is introduced and finally the use of the model is illustrated through simulations and flight verifications. ",
keywords = "Model, Helikopter, Slung load, model, Helicopter, Slung load",
author = "Morten Bisgaard and Bendtsen, {Jan Dimon} and {la Cour-Harbo}, Anders",
year = "2009",
doi = "10.2514/1.36539",
language = "English",
volume = "32",
pages = "573--585",
journal = "Journal of Guidance, Control, and Dynamics",
issn = "0731-5090",
publisher = "American Institute of Aeronautics and Astronautics",
number = "2",

}

Modeling of Generic Slung Load System. / Bisgaard, Morten; Bendtsen, Jan Dimon; la Cour-Harbo, Anders.

I: Journal of Guidance, Control, and Dynamics, Bind 32, Nr. 2, 2009, s. 573-585.

Publikation: Bidrag til tidsskriftTidsskriftartikelForskningpeer review

TY - JOUR

T1 - Modeling of Generic Slung Load System

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AU - Bendtsen, Jan Dimon

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PY - 2009

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N2 - This paper presents the result of the modelling and verification of a generic slung load system using a small-scale helicopter. The model is intended for use in simulation, pilot training, estimation, and control. The model is derived using a redundant coordinate formulation based on Gauss' Principle of Least Constraint using the Udwadia-Kalaba equation and can be used to model all body to body slung load suspension types. The model provides intuitive and easy-to-use means of modelling and simulating different slung load suspension types. It includes detection of, and response to, wire slackening and tightening as well as aerodynamic coupling between the helicopter and the load. Furthermore, it is shown how the model can be easily used for multi-lift systems either with multiple helicopters or multiple loads. A numerical stabilisation algorithm is introduced and finally the use of the model is illustrated through simulations and flight verifications. 

AB - This paper presents the result of the modelling and verification of a generic slung load system using a small-scale helicopter. The model is intended for use in simulation, pilot training, estimation, and control. The model is derived using a redundant coordinate formulation based on Gauss' Principle of Least Constraint using the Udwadia-Kalaba equation and can be used to model all body to body slung load suspension types. The model provides intuitive and easy-to-use means of modelling and simulating different slung load suspension types. It includes detection of, and response to, wire slackening and tightening as well as aerodynamic coupling between the helicopter and the load. Furthermore, it is shown how the model can be easily used for multi-lift systems either with multiple helicopters or multiple loads. A numerical stabilisation algorithm is introduced and finally the use of the model is illustrated through simulations and flight verifications. 

KW - Model

KW - Helikopter

KW - Slung load

KW - model

KW - Helicopter

KW - Slung load

U2 - 10.2514/1.36539

DO - 10.2514/1.36539

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JO - Journal of Guidance, Control, and Dynamics

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