"Quality and Life" № 4(36) 2022. p. 62-66

"Quality and Life" № 4(36) 2022. p. 62-66

Selection of the Effective Payload and Take-off Mass of an Agricultural Unmanned Helicopter

E.A. Basharov, Candidate of Science in Engineering, Associate Professor of Helicopter Design Department, Moscow Aviation Institute (National Research University); Moscow

A.I. Resinets, Doctor of Military Sciences, Associate Professor of Helicopter Design Department, Moscow Aviation Institute (National Research University); Moscow

e-mail: resinetsAI@mai.ru

A.A. Resinets, Assistant at the Aircraft Design and Certification and Helicopter Design departments at the Moscow Aviation Institute (NRU); Moscow

S.A. Tkachenko, Senior Lecturer of Helicopter Design Department, Moscow Aviation Institute (NRU); Moscow

The article analyzes unmanned helicopters of the midi and mini classes and makes a comparative analysis of their characteristics. The selection of the effective payload and take-off mass of agricultural unmanned helicopters should be based on an analysis of the ongoing agricultural work of the future operator.

Keywords: unmanned helicopters, drones, agriculture, on-board electronic equipment, piston engine, turbo-propeller engine, radar.

References:
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5. Beard R.W., McLain T.W. Small Unmanned Aircraft Theory and Practice. Moscow. Technosphere. 2015. 312 p.
6. Izmailov A.Y., Gozhaev Z.A. Project «Creation of a complex of unmanned aerial systems for agricultural purposes». All-Union Research Institute of Agricultural Mechanization, LLC «Geoskan» together with LLC «GIROPLAN RUS». 2016.7
7. Unmanned aircraft. Collection of articles. Avaliable at: UAV.ru.

DOI: 10.34214/2312-5209-2022-36-4-62-66

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