Design and construction of a low-cost test bench for drones
DOI:
https://doi.org/10.29105/ingenierias29.101-991Keywords:
Experimental testing bench, unmanned aerial vehicles, force and moment measurement, load cell instrumentation, low-cost designAbstract
This work presents the design, fabrication, and validation of a low-cost testing bench for measuring forces and moments in all six degrees of freedom (6 DoF) acting on an unmanned aerial vehicle (UAV). The system integrates a strategically arranged set of load cells and a mathematical model that relates sensor signals to the applied loads with respect to the UAV center of gravity. The structural design was developed using CAD and evaluated through numerical analysis, considering components manufactured from polylactic acid (PLA) and aluminum alloy 6061. Experimental results show good agreement with commercial reference sensors, demonstrating the feasibility of an accurate and cost-effective solution for UAV experimental research.
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Copyright (c) 2026 Alejandro Jiménez Flores, Luis Arturo Reyes Osorio, Maria Eugenia Juárez Huitrón, Edmundo Javier Ollervides Vázquez, Octavio García Salazar

This work is licensed under a Creative Commons Attribution 4.0 International License.
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Office of Naval Research Global
Grant numbers N629092512014