Unmanned platforms with a conventional fixed-wing configuration can be designed according to well-assessed aircraft sizing techniques. Conversely, the design of multirotor vehicles is still based mainly on scale-model enthusiastic experience. At present there has been a limited effort by the community in developing a systematic approach for sizing this unconventional class of flying vehicles. This paper proposes a revised version of a classical aircraft sizing methodology based on statistical data available in the literature, with the objective of preliminary sizing of an electric multirotor configuration, taking into account mission profile and a few performance requirements such as endurance or percentage of thrust.
Complete Preliminary Design Methodology for Electric Multirotor
Journal of Aerospace Engineering ; 30 , 5
2017-05-31
Aufsatz (Zeitschrift)
Elektronische Ressource
Unbekannt
Complete Preliminary Design Methodology for Electric Multirotor
Online Contents | 2017
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