Diseño y construcción de un banco de pruebas de bajo costo para drones
DOI:
https://doi.org/10.29105/ingenierias29.101-991Palabras clave:
Banco de pruebas experimental, vehículos aéreos no tripulados, medición de fuerzas y momentos, instrumentación con celdas de carga, diseño y fabricación de bajo costoResumen
Este trabajo presenta el diseño, fabricación y validación de un banco de pruebas de bajo costo para la medición de fuerzas y momentos en los seis grados de libertad (6 DoF) de un vehículo aéreo no tripulado (UAV). El sistema integra un arreglo de celdas de carga configuradas estratégicamente y un modelo matemático que relaciona las señales medidas con las cargas aplicadas respecto al centro de gravedad del vehículo. El diseño estructural se desarrolló mediante CAD y se evaluó mediante análisis numérico, considerando componentes fabricados en PLA y aleación de aluminio 6061. Los resultados experimentales muestran buena concordancia con sensores comerciales, demostrando la viabilidad de una solución precisa y económica para investigación en UAVs.
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Derechos de autor 2026 Alejandro Jiménez Flores, Luis Arturo Reyes Osorio, Maria Eugenia Juárez Huitrón, Edmundo Javier Ollervides Vázquez, Octavio García Salazar

Esta obra está bajo una licencia internacional Creative Commons Atribución 4.0.
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Office of Naval Research Global
Números de la subvención N629092512014