Open AccessConcept for composition of hybrid flying multi-rotor platforms with distributed load and its experimental justification
Author(s) -
V Chemodanov,
K Gavrilin,
Ю. И. Климов,
A. N. Kotel’nikova
Publication year - 2021
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1925/1/012050
Subject(s) - lift (data mining) , rotor (electric) , limit (mathematics) , computer science , energy (signal processing) , energy density , automotive engineering , aerospace engineering , engineering , mechanical engineering , physics , mathematics , engineering physics , mathematical analysis , quantum mechanics , data mining
This paper discusses the main approaches to the development and construction of hybrid flying multi-rotor platforms with separation of lift control functions and angular stabilization functions, called by the authors “distributed load”. A significant factor that limits flight time for majority of multi-rotor platforms is the energy density limit of lithium polymer batteries, which are most commonly used. To solve this problem we analyzed possible ways to increase flight time: replacing the main type of energy carrier for a more energy-intensive one and use of hybrid systems with combination of popular lithium-polymer batteries and a more energy-intensive energy carrier. The analysis was supported by experimental data.