Archivio Istituzionale della RicercaThis paper states a methodology in order to manage the saturation of the propulsion system providing flexibility to the vehicle control unit. To reach this objective a n-copter propeller system is described and a general dispatching law without constrains is found. Furthermore, an optimal propeller problem is proposed and a possible solution using a recursive least squares method is presented.
Saturation managing for the propulsion system and optimal dispatching proposal for multi-rotor UAV / PEREZ MONTENEGRO, CARLOS NORBERTO; Lotufo, MAURICIO ALEJANDRO; Canuto, Enrico; Colangelo, Luigi. - STAMPA. - 1:(2014), pp. 452-457. (Intervento presentato al convegno 2014 IEEE/ASME International Conference on Advanced Intelligent Mechatronics tenutosi a Besancon, France nel 8-11 luglio 2014) [10.1109/AIM.2014.6878119].
Saturation managing for the propulsion system and optimal dispatching proposal for multi-rotor UAV
PEREZ MONTENEGRO, CARLOS NORBERTO;LOTUFO, MAURICIO ALEJANDRO;CANUTO, Enrico;COLANGELO, LUIGI
2014
Abstract
This paper states a methodology in order to manage the saturation of the propulsion system providing flexibility to the vehicle control unit. To reach this objective a n-copter propeller system is described and a general dispatching law without constrains is found. Furthermore, an optimal propeller problem is proposed and a possible solution using a recursive least squares method is presented.
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https://hdl.handle.net/11583/2569339
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