Applications of the Flexible Wing Concept at Small Unmanned Aerial Vehicles

Vasile Prisacariu; Mircea Boscoianu; Ionica Circiu; Cristea Gabriel Rau

doi:10.4028/www.scientific.net/AMR.463-464.1564

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 463-464Applications of the Flexible Wing Concept at Small...

Applications of the Flexible Wing Concept at Small Unmanned Aerial Vehicles

Abstract:

Unmanned Aerial Vehicles have seen a rapid development due to increased miniaturisation of technology, and their multiple usages in both military and civilian fields, thus making this business very profitable. Although the small UAVs are high enabling capabilities, they are still single-role (one flight, one mission). The present paper will present a comparative analysis of the solutions on flexible wing concept and will analyze the possibilities to use the morphing concept at small UAVs.

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Periodical:

Advanced Materials Research (Volumes 463-464)

Pages:

1564-1567

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.463-464.1564

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Online since:

February 2012

Authors:

Vasile Prisacariu, Mircea Boscoianu, Ionica Circiu, Cristea Gabriel Rau

Keywords:

Close-Loop System, Flexibility, Morphing, UAV

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