Preprint Article Version 1 Preserved in Portico This version is not peer-reviewed

Tests of the Tethered Class C3 Hexacopter in Maritime Conditions on the Landing Pad of a Ferry

Version 1 : Received: 3 July 2023 / Approved: 4 July 2023 / Online: 4 July 2023 (11:24:37 CEST)

A peer-reviewed article of this Preprint also exists.

Kownacki, C.; Ambroziak, L.; Ciężkowski, M.; Wolniakowski, A.; Romaniuk, S.; Kulesza, Z.; Bożko, A.; Ołdziej, D. Development and Evaluation of a Tethered Class C3 Hexacopter in Maritime Conditions on the Helipad of a Ferry. Appl. Sci. 2023, 13, 9396. Kownacki, C.; Ambroziak, L.; Ciężkowski, M.; Wolniakowski, A.; Romaniuk, S.; Kulesza, Z.; Bożko, A.; Ołdziej, D. Development and Evaluation of a Tethered Class C3 Hexacopter in Maritime Conditions on the Helipad of a Ferry. Appl. Sci. 2023, 13, 9396.

Abstract

Various UAV applications, especially those based on reconnaissance and observation missions, often require an unlimited time of flight. This is possible only when a UAV is being continuously power supplied from the ground power source, and that is why tethered UAV systems were developed. Tethered UAV systems are based on multicopters which can hover above the landing pad, or track its position in the case it is movable. The presented research is about the development of a large C3 class hexacopter having a maximal payload of about 1 kg, and takeoff mass of 16 kg, which was tested in maritime conditions during the ferry’s cruise. The main purpose of the hexacopter is the continuous observation of the area ahead of a vessel to detect and localize obstacles in the water. During experimental tests critical phases of flight were identified, the AC-DC power supply unit as well as the power cord unwinder were tested, and the power taken by six BLDC motors was registered. The obtained results can be useful in future work on tethered UAV systems used in windy maritime conditions.

Keywords

tethered multicopter; hexacopter; precision landing; moving landing pad; maritime conditions; tether unwinder

Subject

Engineering, Aerospace Engineering

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