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Design of separate lift and thrust hybrid unmanned aerial vehicle

journal contribution
posted on 2024-11-02, 00:44 authored by Puspita Dewi, Ghozali Hadi, Muhammad Kusnaedi, Aris Budiyarto, Agus Budiyono
Hybrid UAV is a new platform of UAV which is integrating fixed wing and multirotor to get vertical takeoff and landing capability with high range and long endurance. Thus it has the benefit of both fixed wing and multirotor platform. The design methodology of hybrid UAV is resembled fixed wing aircraft with modification at some part due to augmentation of multirotor. This Hybrid UAV has been manufactured and on testing phase.

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    ISSN - Is published in 2288582X
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Journal

The Journal of Instrumentation, Automation and Systems

Volume

2

Issue

2

Start page

45

End page

51

Total pages

7

Publisher

UNSYS digital

Language

English

Former Identifier

2006061258

Esploro creation date

2020-06-22

Fedora creation date

2016-04-21

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