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.

References

  1. R. Austin, Unmanned Aircraft Systems: UAVS Design, Development and Deployment, WILLEY, 2010.
  2. "unmannedsystemstechnology.com," Aug 2019. Online. Available: https://www.unmannedsystemstechnology.com/company/elevonx/.
  3. G. o. I. DGCA, "Drone Rules 2021," 2021.
  4. K. A. K. a. K. E. V, "Trends in the development of the global civil drones," Eastern State Transport University, 2018.
  5. Liebeck, Design of the Blended Wing Body Subsonic Transport, Journal of Aircraft, Vol. 41(1), 2004, pp. 10–25.
  6. "The Global Drone Regulation Landscape 2018," Business Insider Intelligence, 2018.
  7. M. H. Sadraey, Design of Unmanned Aerial Systems, WILLEY, 2020.
  8. xflr, "Stability Analysis with XFLR," 2017.
  9. xflr, "Aerodynamic Analysis with XFLR," 2018.

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