Design of folded wing mechanism for Unmanned Aerial Vehicle (UAV)

Unmanned Aerial Vehicles (UAVs) have been widely used both in military and civil all across the world in recent year. Many types of UAV technologies have been developed to answer the global needs, such as for aerial mapping, aerial surveillance, atmospheric sensing, payload delivering, and for war m...

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Bibliographic Details
Main Authors: Anjani Devi, P., Indira priyadarsini, Ch, Avvari, Chandu
Format: Conference Proceeding
Language:English
Subjects:
Motion analysis
SolidWorks
Unmanned Aerial Vehicles
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Summary:Unmanned Aerial Vehicles (UAVs) have been widely used both in military and civil all across the world in recent year. Many types of UAV technologies have been developed to answer the global needs, such as for aerial mapping, aerial surveillance, atmospheric sensing, payload delivering, and for war missions. Most of the UAV are open wing mechanism that causes problem to transport UAVs to other places due to require large space. The main aim of this project is design of folded wing mechanism for small-UAV (
ISSN:2214-7853
2214-7853
DOI:10.1016/j.matpr.2022.04.660