Nuevo vehículo aéreo autónomo estable por construcción: configuración y modelo dinámico

E. Sánchez-Fontes, J.C. Avila Vilchis, A.H. Vilchis-González, B. Saldivar, J.M. Jacinto-Villegas, R. Martínez-Mendez

Resumen

En los últimos años, diferentes estrategias y modelos matemáticos se han desarrollado para analizar y controlar vehículos aéreos no tripulados. Este artículo amplía este panorama al enfocarse en un sistema aéreo no tripulado estable por construcción. Gracias a su diseño, el sistema reportado disipa la energía recibida por la acción de perturbaciones externas. El vehículo propuesto tiene un rotor único para el desarrollo de diferentes modos de vuelo. Este artículo reporta el concepto de diseño del sistema aéreo, la estructura de su modelo dinámico de nueve grados de libertad, un conjunto de simulaciones numéricas que permiten analizar el comportamiento del modelo desarrollado y los primeros resultados experimentales que validan la estabilidad por construcción del vehículo aéreo. Los dos aspectos más significativos e innovadores reportados en este artículo son el uso de un rotor único orientable para la ejecución de diferentes modos de vuelo y la propiedad inherente del sistema que lo hace estable por construcción.


Palabras clave

Estabilidad; Vehículo aéreo no tripulado (UAV); Modelo Dinámico; Actuadores

Clasificación por materias

Robótica y sistemas robotizados; Modelado, identificación, simulación y optimización de sistemas; Control de sistemas de transporte y vehículos

Texto completo:

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Referencias

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