Modelling of Generic Slung Load System

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Resumé

This paper presents the result of 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 gives an intuitive and easy-to-use way of modelling and simulating di erent slung load suspension types and it includes detection and response of wire slacking and tightening, and aerodynamical 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 helicopers or multiple loads. A numerical stabilisation algorithm as well as a trim algorithm is presented for the complete helicopter/load system and finally the use of the model is illustrated through simulations.
OriginalsprogEngelsk
TitelProceedings of the AIAA Modeling and Simulation Technologies Conference and Exhibit
Antal sider20
ForlagAIAA
Publikationsdato2006
ISBN (Trykt)1563478218, 9781563478215
ISBN (Elektronisk)1563478021, 9781563478024
StatusUdgivet - 2006
BegivenhedAIAA Modeling and Simulation Technologies Conference and Exhibit - Keystone, USA
Varighed: 21 aug. 200624 aug. 2006

Konference

KonferenceAIAA Modeling and Simulation Technologies Conference and Exhibit
LandUSA
ByKeystone
Periode21/08/200624/08/2006

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Slings
Helicopters
Stabilization
Wire

Emneord

  • helikopter

Citer dette

Bisgaard, M., Bendtsen, J. D., & La Cour-Harbo, A. (2006). Modelling of Generic Slung Load System. I Proceedings of the AIAA Modeling and Simulation Technologies Conference and Exhibit AIAA.
Bisgaard, Morten ; Bendtsen, Jan Dimon ; La Cour-Harbo, Anders. / Modelling of Generic Slung Load System. Proceedings of the AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA, 2006.
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title = "Modelling of Generic Slung Load System",
abstract = "This paper presents the result of 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 gives an intuitive and easy-to-use way of modelling and simulating di erent slung load suspension types and it includes detection and response of wire slacking and tightening, and aerodynamical 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 helicopers or multiple loads. A numerical stabilisation algorithm as well as a trim algorithm is presented for the complete helicopter/load system and finally the use of the model is illustrated through simulations.",
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Bisgaard, M, Bendtsen, JD & La Cour-Harbo, A 2006, Modelling of Generic Slung Load System. i Proceedings of the AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA, AIAA Modeling and Simulation Technologies Conference and Exhibit, Keystone, USA, 21/08/2006.

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

Proceedings of the AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA, 2006.

Publikation: Bidrag til bog/antologi/rapport/konference proceedingKonferenceartikel i proceedingForskningpeer review

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N2 - This paper presents the result of 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 gives an intuitive and easy-to-use way of modelling and simulating di erent slung load suspension types and it includes detection and response of wire slacking and tightening, and aerodynamical 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 helicopers or multiple loads. A numerical stabilisation algorithm as well as a trim algorithm is presented for the complete helicopter/load system and finally the use of the model is illustrated through simulations.

AB - This paper presents the result of 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 gives an intuitive and easy-to-use way of modelling and simulating di erent slung load suspension types and it includes detection and response of wire slacking and tightening, and aerodynamical 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 helicopers or multiple loads. A numerical stabilisation algorithm as well as a trim algorithm is presented for the complete helicopter/load system and finally the use of the model is illustrated through simulations.

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KW - helicopter

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SN - 1563478218

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Bisgaard M, Bendtsen JD, La Cour-Harbo A. Modelling of Generic Slung Load System. I Proceedings of the AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA. 2006