The cooperative transportation of a cablesuspended load by two rotorcraft is analyzed. First, the equations describing a system made of three point masses and two rigid cables are obtained. Then, the model is linearized about the hovering condition and analytical expressions are derived to describe the eigenstructure of the open-loop system. Based on the particular problem parametrization, the different dynamic modes are discussed with special focus on payload swing. A controller is proposed that allows the agents in the formation to simultaneously perform trajectory-tracking, formation geometry keeping, and payload swing stabilization. Although closedloop stability is preliminary investigated in a linear framework, validation of the approach is performed in a realistic simulation scenario where two multirotors are modeled as rigid bodies under the effect of external disturbances and rotor-generated forces and moments, as obtained by Blade Element Theory. The proposed method has the merit of relative simplicity and is shown to significantly improve vehicle flying qualities of future delivery operations, while minimizing hazardous payload oscillations and reducing energy demand.
Costantini, E., De Angelis, E.L., Giulietti, F. (2024). Cooperative Transportation of a Cable-Suspended Load: Dynamics and Control. 345 E 47TH ST, NEW YORK, NY 10017 USA : IEEE [10.1109/ICUAS60882.2024.10556923].
Cooperative Transportation of a Cable-Suspended Load: Dynamics and Control
Costantini E.
Primo
;De Angelis E. L.
Secondo
;Giulietti F.Ultimo
2024
Abstract
The cooperative transportation of a cablesuspended load by two rotorcraft is analyzed. First, the equations describing a system made of three point masses and two rigid cables are obtained. Then, the model is linearized about the hovering condition and analytical expressions are derived to describe the eigenstructure of the open-loop system. Based on the particular problem parametrization, the different dynamic modes are discussed with special focus on payload swing. A controller is proposed that allows the agents in the formation to simultaneously perform trajectory-tracking, formation geometry keeping, and payload swing stabilization. Although closedloop stability is preliminary investigated in a linear framework, validation of the approach is performed in a realistic simulation scenario where two multirotors are modeled as rigid bodies under the effect of external disturbances and rotor-generated forces and moments, as obtained by Blade Element Theory. The proposed method has the merit of relative simplicity and is shown to significantly improve vehicle flying qualities of future delivery operations, while minimizing hazardous payload oscillations and reducing energy demand.File | Dimensione | Formato | |
---|---|---|---|
icuas_coop_transp.pdf
accesso aperto
Tipo:
Postprint / Author's Accepted Manuscript (AAM) - versione accettata per la pubblicazione dopo la peer-review
Licenza:
Licenza per accesso libero gratuito
Dimensione
1.17 MB
Formato
Adobe PDF
|
1.17 MB | Adobe PDF | Visualizza/Apri |
I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.