Design of Separate Lift and Thrust Hybrid UAV

Authors

  • Puspita Triana Dewi Bhimasena Research and Technology Author
  • Ghozali Suhariyanto Hadi Bhimasena Research and Technology Author
  • Muhammad Ramadhan Kusnaedi Bhimasena Research and Technology Author
  • Aris Budiyarto Bhimasena Research and Technology Author
  • Agus Budiyono Konkuk University Author

DOI:

https://doi.org/10.21535/vz3svt31

Keywords:

hybrid, UAV, VTOL, fixed-wing, multirotor

Abstract

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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Published

2016-01-18