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Comparison of Size and Performance of Small Vertical and Short Takeoff and Landing UAS
  • +1
  • Nicholas Kakavitsas,
  • Andrew Willis,
  • James M Conrad,
  • Artur Wolek
Nicholas Kakavitsas
Department of Mechanical Engineering, University of North Carolina at Charlotte Charlotte

Corresponding Author:[email protected]

Author Profile
Andrew Willis
Department of Electrical and Computer Engineering, University of North
James M Conrad
Department of Electrical and Computer Engineering, University of North
Artur Wolek
Department of Mechanical Engineering, University of North

Abstract

This paper presents a data-set of performance characteristics of nearly two hundred vertical/short takeoff and landing (V/STOL) uncrewed aerial systems (UAS). Characteristics of the UAS that are recorded include maximum gross takeoff weight, endurance, maximum length dimension, speed, payload, and payload fraction. The data-set is restricted to small UAS that weigh under 500 lbs. The results are visualized via scatter plots and statistically characterized. The performance of different UAS design types and UAS Group Numbers are compared. The data-set provides a snapshot of current capabilities of small UAS in the V/STOL category and may be useful to UAS developers and procurement agencies.

Peer review timeline

13 Mar 2024Submitted to TechRxiv
19 Mar 2024Published in TechRxiv