In this paper the authors present a model suitable to convert ultralight airplanes propulsion system from endothermic into electric, focusing only on the power management issues, discarding the mechanical and dynamic ones. The model developed represents a tool to correctly size the propulsion and energy management system of ultra-light aircrafts designed for short endurance flights. The authors performed several experiments to validate the model and to verify the efficiency of the designing tool.
|Titolo:||Design of Solar Powered Ultra-light Aircrafts: Realization of a Model and Its Validation|
|Data di pubblicazione:||2014|
|Appare nelle tipologie:||1.1 Articolo in rivista|