Design and Analysis of High Endurance Fixed Wing Multirotor UAV

Authors

  • Dr. Balaji B  Professor and Head, Department of Mechanical Engineering, K. S School of Engineering and Management, Bangalore, Karnataka, India
  • Dr. Abhishek M R  Associate Professor, Department of Mechanical Engineering, K. S School of Engineering and Management, Bangalore, Karnataka, India
  • Arun V   Research Scolar, Department of Mechanical Engineering, K.S School of Engineering and Management, Bangalore, Karnataka, India

DOI:

https://doi.org//10.32628/IJSRSET229249

Keywords:

UAV, V-TOL, Fixed wing UAV, Solar Hybrid, High Endurance

Abstract

Current work emphasis on research, design and development of a fixed wing multirotor Unmanned Ariel Vehicle (UAV) which operate under V - TOL configuration. In this investigation an effort is made to develop a high endurance and high payload capacity UAV which can have a payload capacity of 15 Kg and which can serve with the endurance of 2 hrs per cycle.

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International Journal of Scientific Research in Science, Engineering and Technology

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Published

2022-04-30

Issue

Volume 9, Issue 2, March-April-2022

Section

Research Articles

License

Copyright (c) IJSRSET

Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

How to Cite

[1]
Dr. Balaji B, Dr. Abhishek M R, Arun V , " Design and Analysis of High Endurance Fixed Wing Multirotor UAV, International Journal of Scientific Research in Science, Engineering and Technology(IJSRSET), Print ISSN : 2395-1990, Online ISSN : 2394-4099, Volume 9, Issue 2, pp.277-287, March-April-2022. Available at doi : https://doi.org/10.32628/IJSRSET229249