A 55-pound Vertical-Takeoff-and-Landing Fixed-Wing sUAS for Science: Systems, Payload, Safety Authorization, and High-Altitude Flight Performance-Reference-Cited by-同舟云学术

A 55-pound Vertical-Takeoff-and-Landing Fixed-Wing sUAS for Science: Systems, Payload, Safety Authorization, and High-Altitude Flight Performance

Published:2022-06-21 Issue: Volume: Page:
ISSN:
Container-title:2022 International Conference on Unmanned Aircraft Systems (ICUAS)
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Author:

Coopmans Calvin¹,Slack Stockton,Robinson Daniel J.,Schwemmer Nathan

Affiliation:

1. Utah State University,Utah Water Research Laboratory and the Electrical and Computer Engineering Department,Logan,UT,84321

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9836022/9835714/09836128.pdf?arnumber=9836128

Reference23 articles.

1. Research on application mode of large fixed-wing UAV system on overhead transmission line;wu;2017 IEEE International Conference on Unmanned Systems (ICUS),2017

2. Aerodynamics and Structure of a Large UAV;vestlund;Master’s thesis,2018

3. Avionics subsystems design and development for HALE UAV ITB V4

4. An Unmanned Aerial Vehicle Sampling Platform for Atmospheric Water Vapor Isotopes in Polar Environments;rozmiarek;Atmospheric Measurement Techniques Discussions,2021

5. Design Methodology for Heavy-Lift Unmanned Aerial Vehicles with Coaxial Rotors

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