Show simple item record

contributor authorHünteler, Carlos
contributor authorSaweeres, Fady
contributor authorRupprecht, Tim
contributor authorHolzapfel, Florian
date accessioned2026-08-23T07:59:33Z
date available2026-08-23T07:59:33Z
date copyright2026/04/01
date issued2026
identifier issn2689-6117
identifier otheraldsc-25-1056.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4315913
description abstractAbstract. The powertrain design is crucial for success in the electric multirotor aircraft development race. It significantly impacts the aircraft’s performance, maneuverability, and safety. The sizing of all powertrain components is essential for balancing efficiency, and dynamics within its entire operational envelope. This work proposes a holistic approach to analyze the dynamics of a powertrain by considering the most relevant components, including the batteries, the electronic speed controller, the motor, and the propeller. The entire powertrain is formulated as a first-order system which is examined via a phase plane analysis. This facilitates the assessment of the underlying dynamics on a rotational rate of change and thrust rate of change degree for every operating condition. Moreover, the whole operational envelope of the powertrain is displayed, including the subsystems’ physical constraints. This results in an accurate performance prediction and acts as an enabler for effective control strategies as well as for future design optimizations.
publisherThe American Society of Mechanical Engineers (ASME)
titleHolistic Analysis of Electric Aircraft Powertrain Dynamics
typeJournal Paper
journal volume6
journal issue2
journal titleASME Letters in Dynamic Systems and Control
identifier doi10.1115/1.4070253
journal fristpage321
journal lastpage329
page9
treeASME Letters in Dynamic Systems and Control:;2026:;volume( 006 ):;issue:002
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record