Experimental measurement data was obtained utilizing RCbenchmark 1780 with full-range PWM signals. Measurements were made for two series of setups.

First series is related to low-voltage setups using the following T-MOTOR components: - motors: MN4014 400Kv, MN5212 340Kv, MN501-S 360Kv, U7 280Kv, MN6007 320Kv, P60 340Kv, MN701-S 280Kv; - ESC: Air 40A, Flame 40A, Flame 70A, Alpha 60A, Flame 100A; - propellers: P17×5.8, P18×6.1, P20×6, P22×6.6, P24×7.2, G26×8.5; - battery: 6-cell (6S) Lithium polymer (LiPo).

DOI Link: 
10.21227/pvq1-tv90
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[1] Denis Kotarski, "Heavy Lift Multirotor UAV - Electric Propulsion Unit Experimental Data", IEEE Dataport, 2023. [Online]. Available: http://dx.doi.org/10.21227/pvq1-tv90. Accessed: Dec. 13, 2024.
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doi = {10.21227/pvq1-tv90},
url = {http://dx.doi.org/10.21227/pvq1-tv90},
author = {Denis Kotarski },
publisher = {IEEE Dataport},
title = {Heavy Lift Multirotor UAV - Electric Propulsion Unit Experimental Data},
year = {2023} }
TY - DATA
T1 - Heavy Lift Multirotor UAV - Electric Propulsion Unit Experimental Data
AU - Denis Kotarski
PY - 2023
PB - IEEE Dataport
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Denis Kotarski. (2023). Heavy Lift Multirotor UAV - Electric Propulsion Unit Experimental Data. IEEE Dataport. http://dx.doi.org/10.21227/pvq1-tv90
Denis Kotarski, 2023. Heavy Lift Multirotor UAV - Electric Propulsion Unit Experimental Data. Available at: http://dx.doi.org/10.21227/pvq1-tv90.
Denis Kotarski. (2023). "Heavy Lift Multirotor UAV - Electric Propulsion Unit Experimental Data." Web.
1. Denis Kotarski. Heavy Lift Multirotor UAV - Electric Propulsion Unit Experimental Data [Internet]. IEEE Dataport; 2023. Available from : http://dx.doi.org/10.21227/pvq1-tv90
Denis Kotarski. "Heavy Lift Multirotor UAV - Electric Propulsion Unit Experimental Data." doi: 10.21227/pvq1-tv90